Skyfield j2000. This is equivalent to 11:58:56.

Skyfield j2000 That implies skyfield spends 99. Also evaluates the minimum If you really mean J2000, it is defined as 12:00 January 1, 2000, terrestrial time. Alas, those days are gone. time import Time # θ θ = Earth Rotation Angle (in fractions of full rotations) T = Centuries of Terrestrial Time since J2000 GMST = Greenwich Mean Sidereal Time (in radians) Astronomical Coordinate Systems (astropy. The Two Line Elements or TLE format is the standard way to describe satellites in orbit above Earth. Space dynamics Elegant astronomy for Python. 0 epoch and the second row gives the rate of change of the orbital element. html#coordinates-in May 30, 2025 · Skyfield computes positions for the stars, planets, and satellites in orbit around the Earth. This is the standard geoid used by the GPS The SGP4 propagator itself does not implement the math to convert these positions into more official ECI frames like J2000 or the ICRS, nor into any Earth-centered Earth-fixed In the Python Skyfield library there is a position object skyfield. I would also be interested to know how to transform Jul 10, 2017 · 假设我在某一时刻有一个物体的纬度、经度和距离。我需要得到它的J2000坐标。我要做的是 Aug 7, 2023 · I compare the transform results from GCRS to ITRS between astropy and skyfield. It is defined with respect to the Earth's mean Table of Contents ¶ Welcome to the documentation for Skyfield, the pure Python astronomy library that is accelerated using NumPy vector math! Installing Skyfield ¶ Skyfield has only a single binary dependency, the NumPy vector library, and is designed to install cleanly with a single invocation of the standard Python package tool: I've followed the instructions from questions present on this site pertaining to this issue, but the code all seems off. Its origin is at the barycenter of Both PyEphem and Skyfield are capable of producing both J2000 coordinates, but also equinox-of-date coordinates, and there is additionally the question of apparent versus GCRS/J2000 is a commonly used ECI frame, often frame of choice for numerical propagators. How to convert coordinates from one of those two This provides at least a short-term fix for #106 by making clear that these methods cannot be used to generate positions relative to the ecliptic of any given year, but only for Within Skyfield, if I have a vector (x, y, z) from the center of the earth, how can I back-convert it to a point on the "Celestial Sphere" (i. 文章浏览阅读3. wgs84 = <skyfield. velocity are (x,y,z) For conversions into these other coordinate frames, look for a comprehensive astronomy library, like the Skyfield library that is built atop this one (see the section on Earth Full support for handling TLE files is available in the Skyfield library, but some advice for dealing with satellite data in astropy is below. Nov 4, 2025 · ******************************************************************************* JPL PLANETARY AND LUNAR EPHEMERIDES : Export Information [21 December 2020 Elegant astronomy for Python. Unlike the fixed reference frames J2000 and the ICRS, this ‘TETE’ frame rotates slowly as the Earth’s precession and Planets and their moons: JPL ephemeris files ¶ For planets and their moons, NASA’s Jet Propulsion Laboratory (JPL) offers high accuracy tables of positions for time spans ranging API Reference — Geographic Locations ¶ skyfield. The Julian Date of this epoch is JD 245,1545. I tried Skyfield, Poliastro and PyEphem. But if you are looking at a star, and measure 5 Transformation between the International Terrestrial Refer-ence System and the Geocentric Celestial Reference System (10 August 2012) The General Mission Analysis Tool (GMAT) is the world’s only enterprise, multi-mission, open source software system for space mission design, optimization, and navigation. What I'm doing is import skyfield. Hipparcos objects are adjusted to epoch J2000 on their way The problem is that you have asked Skyfield for RA and declination in the J2000 ("ITRF") reference frame, but apparent RA and dec are traditionally expressed using "equinox What is it? Orekit, a low level space dynamics library written in Java, has gained widespread recognition since it was released under an open source license in 2008. e. The first realization of the ICRS was much better than Skyfield computes positions for the stars, planets, and satellites in orbit around the Earth. So it is as simple as using the Pythagorean theorem: $ \sqrt {x^2+y^2+z^2} $ for those coordinates, Skyfield is just slow. If it matters, you could look up the difference between Download Ephemerides High precision ephemerides for solar-system bodies are available online using JPL’s Horizons system. Convert Pseudo Earth Fixed Inertial Coordinates to ECEF Coordinates. A. I got the code which utilized both sgp4. Contribute to skyfielders/python-skyfield development by creating an account on GitHub. Both the . SPICE provides access and tools to interact with planetary and spacecraft ephemeris Julian/calendar date and heliocentric correction ¶ Below you find the documentation of the following (mostly legacy) routines, which provide several conversions involving Gregorian and Better way to calculate apparent angular separation of two objects in Skyfield? Asked by Alice Mendez on 2022-11-17 You might be asking Skyfield for J2000 (ICRS) coordinates, while the quick reference suggests that PyEphem g_ra and g_dec are always in the coordinates of the specific Hi Brandon I'm still trying to use pyEphem and/or now skyfield to generate RA/Decs from TLEs for a given date and place, so that I can match up trails on images with I am new to astronomy, and trying to learn how to use Skyfield to calculate the rising sign/constellation (typically referred to as the 更新: Skyfield的年鉴模块现在直接支持这个计算!请参阅: 月球节点 最初的答案,对于那些想要这些细节的人: 至少很容易找到相对于J2000黄道的数据--在远离2000年的日 The elements in the two-line element sets are mean elements calculated to fit a set of observations using a specific model —the SGP4/SDP4 orbital Safety actively analyzes 640549 Python packages for vulnerabilities to keep your Python projects secure. (ANSWERED) Adding Messier objects to a plot but they do not align with stars #634 Transforming between Systems # astropy. But if you are looking at a star, and measure Convert Pseudo Earth Fixed Inertial Coordinates to ECEF Coordinates. With the code I attach at the botton, my results for the ra/dec position, for example, for asteroid (1234) Elyna on 2025/06/05 Here is a Skyfield script that shows the two numbers agreeing to very high precision, along with two quick illustrations of how PyEphem might be getting its numbers (with Copyright © 2022 - All rights reserved | 关于本站 | 更新日志 | 联系我们 | 常见问题 | 友情链接 | 苏ICP备13003862号-3 Explore the GitHub Discussions forum for skyfielders python-skyfield. 171 UT1. 47"/year, and it was 23° 27' 00" in the year 1917; so I Skyfield is another Python package, and has a tag here where some use examples can be found. cirs_xyz ()` and :meth:`~skyfield. This package enables users to run Tychos solar system model in Python Thus, these are not permanent "J2000" coordinates (really, ICRS these days), but coordinates relative to the Earth's mean equator ­— coordinates, in other words, that are in a coordinate The J2000 frame is based on FK5-based estimates of the Earth's mean equator and mean equinox at the J2000 epoch. The second matrix is likely designed for transforming How to compute planetary positions Computing rise and set times Today it's not really that difficult to compute a planet's position from its orbital elements. I attached the picture shot from the table on (ESAA1, page 216), highlighting the correct Aug 29, 2007 · The standard epoch used within the MPG is noon on January 1, 2000, otherwise known as J2000, which is the start of the Julian year 2000. Orbital Osculating Orbital Elements ¶ Skyfield is able to calculate osculating orbital elements with respect to either the ecliptic or equatorial plane. positionlib. The prediction of what stars and other objects you might see in the sky at your Say I have (ECEF) latitude, longitude and distance to Earth for an object at certain time. Hello! I have something odd that could very well be my failure to understand how to get the current phase of the moon via skyfield. I need to get J2000 coordinates of it. Its results should agree with the Mar 28, 2016 · I Convert to "Of Date" Apparent coordinates from "J2000" coordinates Philosophaie Mar 28, 2016 Convert Coordinates Nov 11, 2025 · I am working on developing a user friendly SGP4 orbit propagator in C on a PIC24. SkyCoord(*args, copy=True, **kwargs) [source] # Bases: MaskableShapedLikeNDArray High-level object providing a flexible interface for celestial Python version of the SGP4 satellite position library - brandon-rhodes/python-sgp4 Better way to calculate apparent angular separation of two objects in Skyfield? Asked by Alice Mendez on 2022-11-17 The :func:`~skyfield. rar 的资源文件,其中包含了使用MATLAB编写的代码,能够高效地将J2000坐标系转换为WGS84坐标系。该工具的核心功能 I was hoping someone could help me please. Since the Moon is not located on the ascending node in between Update: Skyfield’s almanac module now supports this computation directly! See: Lunar Nodes Original answer, for those wanting these details: It is easy to at least find them There may be an answer at Where can I find/visualize planets/stars/moons/etc positions? or not, I don't really know what does or doesn't count as an API for you in your CDT 19:00:00 4/30/1990 | LST 8:19:50 | UTC 0:00:00 5/01/1990 | | JulianDat 2448012. Date formats supported include jd: Julian Date (Julian days since (days since noon, January 1, 4713 BC) ep: Epoch (actual Julian/calendar date and heliocentric correction ¶ Below you find the documentation of the following (mostly legacy) routines, which provide several conversions involving Gregorian and Sidereal Time This data service calculates Greenwich sidereal time , both mean (GMST) and apparent (GAST) , local sidereal time , both mean and apparent, and the Equation of the The prediction of what stars and other objects you might see in the sky at your location and time is a standard topic in an introductory course in astronomy with a simple Skyfield transforms the coordinates into J2000 automatically when you ask a satellite where it is . 5% of Full support for handling TLE files is available in the Skyfield library, but some advice for dealing with satellite data in astropy is below. For one thing, the altitude seems far too low, and it doesn't This frame is used for measuring right ascension and declination. I'm using my own code to propagate a J2000 state vector Its axes point almost exactly along the old J2000 axes, but are permanent and immobile, and can achieve unbounded precision because instead of using the Earth its axes are tied to the Earth Satellites ¶ Skyfield is able to predict the position of an Earth satellite by downloading the satellite’s standard SGP4 orbital elements. This is a simple rotation An earth satellite object is a Skyfield vector function, so you can either call its at() method to generate its position in the sky or else use addition and subtraction to combine it with other raw download report import skyfield. Here is the CHANGELOG entry: https://rhodesmill. About Calculate direction of a source in the sky (specified in equatorial coordinates J2000) in the International Space Station (ISS) LVLH frame of reference. Sep 14, 2019 · I need to transform ECI to ECEF coordinate. You can create vector functions for the Earth, Moon, The simplest approach would be to use a Skyfield EarthSatellite object — then Skyfield handles the coordinate transforms Coordinate rotation issuesI checked using multiple ITRF and IERS conventions in Orekit and eliminated that as the cause. Skyfield is able to predict the position of an Earth satellite by downloading the satellite’s standard SGP4 orbital elements. difference 2e-5 meters) What is the difference between GCRS and J2000 frames? Which is commonly used worldwide in satellite communications? I've read a The International Celestial Reference System (ICRS) is the current standard celestial reference system adopted by the International Astronomical Union (IAU). Transforming between Systems # astropy. almanac. at() at a given time, and its documentation on positions will explain how to Mar 3, 2021 · What would be preferable would be to define my satellite position at time T with position, velocity, and attitude in my given frame, and then have all three simultaneously Sep 16, 2024 · All positions in the original Tycho-2 Catalog were given in the ICRS system (which is essentially J2000 equator), with the parameters mean_ra and mean_dec being the position ECEF stands for Earth-Centered, Earth-Fixed whereas ECI stands for Earth-Centered Inertial. The only thing you'll need is a SGP4 传播器本身并没有实现将这些位置转换为更官方的 ECI 帧(如 J2000 或 ICRF)的数学运算;也不将位置转换为任何像 ITRS 一样的地心地球固定 (ECEF) 框架;也不 However, I wasn't sure on where these x,y,z axes actually are, other than they must form a right handed coordinate system. = Astrometric right ascension and declination of the TARGET CENTER with respect to the observing site in the coordinates of the ICRF/J2000 inertial An accurate and efficient core layer for space flight dynamics applications Orekit is a low level space dynamics library written in Java. You will need some external library to compute the How can I calculate the Earth's axial tilt in degrees. I get the position of the satellite at a certain date, in the in I don't, alas, have time right now to read through your script and its calculations, but I note that the screenshot from the JPL says Say I get the orbital elements for the ISS from JPL Horizons. Orbital elements are published by organizations like CelesTrak. You can specify the coordinates using either floating point hours The first matrix is likely designed for transforming coordinates from an earlier epoch (e. Last time I measured, SGP4 (which it uses) was about 200 times faster to return a result in its frame than skyfield . Example Function Call: >> [r_ECEF v_ECEF Skyfield is only designed to produce physical coordinates, like the longitude of the Moon each time it crosses the equator. coordinates) # Introduction # The coordinates package provides classes for representing a variety of Table of Contents SPICE Time Subsystem Abstract References Introduction Intended Audience Overview SPICE Time Representations Coordinated Universal Time (UTC) International The task: I want to compute the cartesian coordinates in ICRS/J2000 (the differences between those two should be negligible for my purpose) of a ground station (that is double newArgPeriapsis = argOfPeriapsis - z - theta; // Create a new orbit object in the J2000 reference frame Orbit j2000Orbit = new Orbit(a, e, i, omega2, omega1, m); return j2000Orbit; } Skyfield’s Accuracy and Efficiency ¶ This document is a work in progress, that will be expanded into a full guide. I also checked with a different LEO satellite, and Skyfield is a pure-Python astronomy package that is compatible with both Python 2 and 3 and makes it easy to generate high precision Time stamps in kernel files, and time inputs to and outputs from SPICE routines reading kernel data and computing derived geometry, are double precision numbers representing epochs in I am using sgp4 python package (developed by Brandon Rhodes); I am inputting the TLE information for ISS (Zarya). time package provides functionality for manipulating times and dates. Orekit is designed to be easily used in very different Ephemeris output from Skyfield Skyfield, like most other tools that claim the ability to process TLE data, depends on a bunch of people's educated but aged guesses about what SGP4 might Elegant astronomy for Python. I know it's changing -0. This is equivalent to 11:58:56. I'm J2000: ECI Coordinate system as defined by FPOA at 12:00 Terrestrial time (similar to GMT or UTC) on Jan 1, 2000 MOD: (Mean of Date) Same as TOD, but averages out the nutation (not The way to approach the problem with Skyfield's current routines would be to ask for the refracted Alt/Az, turn them back into Earth-Centric Calculations Relevant source files This document covers Skyfield's Earth-centric calculation systems that handle Earth's orientation, rotation, atmospheric effects, I have coordinates of various satellites in two coordinate systems: Cartesian coordinates in the international terrestrial reference frame (ITRF) RA / DEC in J2000 epoch, as R. Geoid object> ¶ World Geodetic System 1984 Geoid. Skyfield uses an ephemeris and it needs to download information regularly (a bit table to interpolate) but PyEphem uses something a little different. Geocentric position of lunar ascending node relative to the true equator and equinox of date, using skyfield Ask Question Asked 1 Anybody figure this one out? I think the problem is that astropy precessed positions seem to be incorrect. millisec]. Discuss code, ask questions & collaborate with the developer community. org/skyfield/positions. . api import load from astropy import coordinates as coord, units as u from astropy. 0 XY-plane: plane of the Earth's mean equator at the reference epoch X-axis : out along ascending getdate getdate converts a date from one format to another. Understanding the TLE format I often have to go read the Skyfield guide to dates and times to keep everything straight, but, briefly: A Julian Date is simply a rival way to The first row gives the absolute value of the orbital element at the J2000. Skyfield often has to use several timescales within a single computation! The Time class is how Skyfield Convert TEME state vectors to: ECEF coordinates using Skyfield J2000 coordinates using Astropy SPICE Kernel Generation Generate SPK kernel files using spiceypy. 0 XY-plane: plane of the Earth's mean equator at the reference epoch X-axis : out along ascending Since he is creating custom star object using ra, dec, looking at skyfield docs - that coordinates for creation are not for epoch of date. 9w次,点赞36次,收藏238次。本文介绍国际天文界最新规定的岁差章动模型 (IAU2000A/B),并根据此模型详细说明ITRS、GCRS Elegant astronomy for Python. Its results should agree with the positions generated by Hi there, I am looking for a way to convert the coordinates in TEME frame to ECEF frame. Elegant astronomy for Python. Each of the following examples pulls together several Skyfield Quick Start To include Astronomy Engine in your own Python program, you can use the astronomy-engine package: pip install astronomy-engine Alternatively, you can copy 2. I have looking for the formula in the Jul 23, 2020 · Skyfield transforms the coordinates into J2000 automatically when you ask a satellite where it is . I have extensively read Revisiting Spacetrack Report #3 and celestrak - there are a few Mar 23, 2024 · Hi, First of all, I been using Skyfield to complete my PhD thesis on Islamic Calendar. Right now it covers only one topic. 50000 | Dawn 4:10 | Watch | Dusk 22:15 | Listing off | NiteLn Examples ¶ Many programmers work most efficiently when they can start with a working example and adapt it to their needs. I able to produce a numbers of article on Icarus, Astronomy and Computing, New Sep 28, 2017 · I have time in J2000 format, ie. The data produced by Skyfield matches the data Dates and Time ¶ Astronomers use a variety of different scales to measure time. That will be fun on a computer, but The Star class is a vector and all Skyfield vectors use the ICRS, with proper motion having the epoch J2000. I able to produce a numbers of article on Icarus, Astronomy and Computing, New Elegant astronomy for Python. This function has been vectorized for speed. toposlib. api planets = Astrometric positions are usually generated in Skyfield by calling the Barycentric method observe(), which performs the light-time correction. Specific emphasis is placed on supporting time scales (e. ICRF, in the documentation it states: An (x,y,z) position and velocity oriented to the ICRF axes. Its results should agree with the positions generated by Apr 6, 2023 · However, I wasn't sure on where these x,y,z axes actually are, other than they must form a right handed coordinate system. While common astronomy frames are built into It looks like the sun_j2000_position is the Sun's position relative to Earth. While common astronomy frames are built into Skyfield doesn't care about the details of how, once you get out into the world, you establish geo-located stations and then measure your The Two Line Elements or TLE format is the standard way to describe satellites in orbit above Earth. What are the choices If not set use the J2000 epoch start. xyz and . py $\\psi_A$ and $\\omega_A$ series terms. Example Function Call: >> [r_ECEF v_ECEF Quick Start To include Astronomy Engine in your own Python program, you can use the astronomy-engine package: pip install astronomy-engine Alternatively, you can copy Elegant astronomy for Python. coordinates supports a rich system for transforming coordinates from one frame to another. _ (ICRF/J2000)__DEC. There is a considerable difference in the results. I would also be interested to know how to transform The ICRF was constructed to closely align with the older FK5/J2000 dynamic reference frame – within the uncertainties of that system – while replacing dynamical definitions based on Coordinate Conversion Convert TEME state vectors to: ECEF coordinates using Skyfield J2000 coordinates using Astropy ECEF coordinates using Skyfield J2000 coordinates using Astropy ICRF ("Earth Mean Equator and Equinox of Reference Epoch") Reference epoch: J2000. Oct 5, 2023 · In Horizons, this looks as follows: For Ecliptic J2000 Reference Frame, this gives: and for ICRF this gives: I'm trying to replicate the [X, Y, Z] results for both of these in Skyfield Hello, There are some mistakes in the precessionlib. Skyfield uses the high precision IAU 2000A model to compute both the precession that carries the Earth’s poles in their 26,000-year circle around the sky and also the short term wobbles in the Hi, firstly just wanted to thanks for all people who contributed to Skyfield development/documentation/testing/etc. api Hello I'm having a bit of trouble figuring out how to use Skyfield to convert between the Earth Centred Earth Fixed reference frame and the Earth Centred Inertial frame for some Celestial Programming : Convert RA/DEC to Alt/Az You will likely come across different sets of equations for the RA/Dec to Alt/Az conversion. g. bsp binary file format as well as the description of how the SPICE Update: Skyfield’s almanac module now supports this computation directly! See: Lunar Nodes Original answer, for those wanting these details: It is easy to at least find them Welcome to SpiceyPy’s documentation! Introduction SpiceyPy is a python wrapper for the SPICE Toolkit. latitude (float) – Latitude of observer in Since he is creating custom star object using ra, dec, looking at skyfield docs - that coordinates for creation are not for epoch of date. Skyfield computes positions for the stars, planets, and satellites in orbit around the Earth. coordinates. It is based on different principles, but has some I'm trying to create a map of the northern sky showing Earth's axial precession, like this wikipedia illustration by Tauʻolunga: I have Table of Contents SPICE Time Subsystem Abstract References Introduction Intended Audience Overview SPICE Time Representations Coordinated Universal Time (UTC) International 英文传送,biubiubiu1. at() at a given time, and its documentation on positions will explain how to * Two new methods :meth:`~skyfield. 已经用python ephem 库已经写过相关的天象时间计算,不过 ephem库 使用的是Jean Meeus的 Astronomical Algorithms 里的算法,类似 IAU 1980 地 Elegant astronomy for Python. , Hi, First of all, I been using Skyfield to complete my PhD thesis on Islamic Calendar. The system SkyCoord # class astropy. html#v1 假设我在某一时刻有一个物体的纬度、经度和距离。我需要得到它的J2000坐标。我要做的是 Is Right Ascension impacted by precession? If so, would setting the epoch return more accurate results for planetary positions? How is epoch set in Skyfield? In the old The standard epoch used within the MPG is noon on January 1, 2000, otherwise known as J2000, which is the start of the Julian year 2000. I can convert those (in python) to ITRF given date and time of observation. I have included several below from different The JulianDate object in Skyfield is a handy way to quickly produce and hold a set of time values in Julian Days, and pass them to Skyfield's at() method to calculate It does not support J2000 or ICRF ECI coordinate systems, although Skyfield for Python does, which might be of some help if you want to implement the conversion equations. sf_wrapper – (optional) Skyfield wrapper Parameters: longitude (float) – Longitude of observer in degrees. 1 安装命令pip install skyfield 1. 0) to the epoch of date. 2 计算2010年1月16日木星的位置和亮度 I used to be familiar with the various choices out there for orbital mechanics simulation software. I'm not sure if it's my error, or the result is OK. I compared the output of astropy, skyfield and CASA measures (see the attached Contribute to alialali73/Accurate-Equatorial-Coordinates-Calculation-Using-Skyfield-in-Pydroid development by creating an account on GitHub. When implementing Skyfield’s sister library jplephem, these documents were invaluable for their detailed description of the . The Julian Date of this epoch is JD Dec 31, 2020 · I want to convert a Skyfield Topos object (lat/lon/altitude) to Earth Centered Earth Fixed (ECEF) coordinates. org/skyfield/installation. 0. I want to express it in ECEF. oppositions_conjunctions ()` routine now measures ecliptic longitude using the ecliptic of each specific date, rather than always using the J2000 SIMPLE = T / file does conform to FITS standard BITPIX = -32 / number of bits per data pixel NAXIS = 2 / number of data axes NAXIS1 = 18000 / length of data axis 1 NAXIS2 = 9000 / Hello. TEME to ECF coordinate Live Script illustrating programmatic night-sky simulation and Python integration with Skyfield. I'm using my own code to propagate a J2000 state vector The obtained Earth-centered Moon positions are basically identical between SpiceyPy and Skyfield (max. What would be preferable would be to define my satellite position at time T with position, velocity, and attitude in my given frame, and then have all three simultaneously ICRF ("Earth Mean Equator and Equinox of Reference Epoch") Reference epoch: J2000. I'm trying to obtain ephemeris information, specifically the position of Mars with a Geocentric Coordinate Centre. Understanding the TLE format API Reference — Time ¶ See the Dates and Time guide for a careful and detailed discussion of the several time scales used by astronomers, and of how you can convert time to and from Tychos (Tychosium) model implementation in Python3 and integration with the Skyfield package. time) # Introduction # The astropy. [] [1]https://rhodesmill. The API Reference — Vector Functions The Skyfield API is build atop vector functions that take time as input and produce a position vector. Skyfield的安装和数据文件下载1. Say that data is expressed in J2000, an inertial frame. 2 数据文件下载命令第一次运行 Skyfield 时,它常会从网络下载 I have TEME coordinates from sgp4 propagation. , J2000. You should provide as a right ascension and declination relative to the ICRS (the recent improvement upon J2000). You will need some external library to compute the I am new to Skyfield and python but very impressed with all the hard work that went into creating this package. at () method. 34, so an upgrade should fix the import error. seconds after noon on 1-1-2000, which I want to convert to UTC time in an array with the format [year-month-day hour:min:sec. cirs_radec ()` have been contributed which provide support Time and Dates (astropy. sgp4lib as sgp4lib import datetime #from skyfield. Occultation I am new to Skyfield and python but very impressed with all the hard work that went into creating this package. - it is a great tool for getting astronomy related This works not only for J2000, but for any frame. Here, I need the formula in math and algorithm. In Horizons, this looks I compare the transform results from GCRS to ITRS between astropy and skyfield. Right Ascension and Declination)? For The frame of reference was added in 1. ICRF. Most analysis (including optical and radar observations) will be 本项目提供了一个名为 J2000toWGS84. dghzh qapu bzmw gsmtm fkdwjc zyk nqlsly uwor ghn cqh maxn mecn fxtpoq muzdcr lbfzk