XINGYUN-2 02, 45603
Orbit data source: Space-Track
XINGYUN-2 02, 45603 is a payload satellite owned by Xingyun (CN) in SSO that was launched on Tue, 12 May 2020 UTC via a KUAIZHOU-1A launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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45603 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Sanjiang
Mission
Operational Commercial Communications
Bus & Motor
XINGYUN, Unknown motor
Mass
93 kg wet, ~85 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.4 m
Radar Cross Section
0.569 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 XINGYUN-2 02
1 45603U 20028B 26316.84673909 .00001051 00000-0 64804-4 0 9997
2 45603 97.5102 320.3110 0012348 115.4177 244.8333 15.12030054357292Epoch: 2026-11-12T20:19Z
TLE epoch observation values (Epoch: 2026-11-12T20:19:18.257Z)
Latitude
-0.00001°
Longitude
-36.48944°
Altitude
536.723 km
Speed
7.592 km/s
True Right ascension
21h 21m 14s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
21:58:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
535.517 km
Perigee altitude
518.464 km
Semi-major axis
6,905.128 km
Eccentricity
0.00123
Inclination
97.5102°
RAAN
320.311°
Arg. of periapsis
115.4177°
True anomaly
244.70532°
Mean anomaly
244.8333°
Eccentric anomaly
244.7693°
Mean motion
3.78256 °/min
Orbital period
95.17 mins
BSTAR
0.000064804
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Other satellites on launch #28 in the year 2020 (2020-05-12 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.XINGYUN-2 02 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-11-13 12:46:26.397Z | 33.299° NE | 2026-11-13 12:49:26.397Z | 97.583° ESE | 36.128° | 2026-11-13 12:52:26.397Z | 162.449° S |
| 4 mins | 2026-11-13 23:29:26.397Z | 94.526° ESE | 2026-11-13 23:30:26.397Z | 76.048° E | 17.488° | 2026-11-13 23:33:26.397Z | 24.92° NE |
| 4 mins | 2026-11-14 01:03:26.397Z | 223.113° SW | 2026-11-14 01:05:26.397Z | 278.32° WNW | 29.014° | 2026-11-14 01:07:26.397Z | 317.613° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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