XINGYUN-2 01, 45602
Orbit data source: Space-Track
XINGYUN-2 01, 45602 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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45602 intel report (Beta)
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Edit Public Description
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, Unknown HBR
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 01
1 45602U 20028A 25321.85603094 .00004394 00000-0 27022-3 0 9993
2 45602 97.4755 313.8046 0008466 201.7979 158.2892 15.10517517302924Epoch: 2025-11-17T20:32Z
TLE epoch observation values (Epoch: 2025-11-17T20:32:41.073Z)
Latitude
0.00002°
Longitude
-51.51701°
Altitude
543.135 km
Speed
7.588 km/s
True Right ascension
20h 55m 13s
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
21:56:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
537.452 km
Perigee altitude
525.752 km
Semi-major axis
6,909.739 km
Eccentricity
0.00085
Inclination
97.4755°
RAAN
313.8046°
Arg. of periapsis
201.7979°
True anomaly
158.32505°
Mean anomaly
158.2892°
Eccentric anomaly
158.30713°
Mean motion
3.77877 °/min
Orbital period
95.27 mins
BSTAR
0.00027022
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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 01 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-11-18 11:26:32.774Z | 58.687° ENE | 2025-11-18 11:28:32.774Z | 90.731° ESE | 14.102° | 2025-11-18 11:30:32.774Z | 123.789° SE |
| 5 mins | 2025-11-18 13:01:32.774Z | 334.964° NNW | 2025-11-18 13:03:32.774Z | 274.81° WNW | 29.603° | 2025-11-18 13:06:32.774Z | 222.089° SW |
| 6 mins | 2025-11-18 23:42:32.774Z | 171.092° S | 2025-11-18 23:44:32.774Z | 187.265° SSW | 42.941° | 2025-11-18 23:48:32.774Z | 346.086° N |
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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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