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: 1 day ago
TLE from 1 day ago
0 XINGYUN-2 01
1 45602U 20028A 25306.48653351 .00002857 00000-0 17780-3 0 9998
2 45602 97.4750 298.7994 0007524 264.3605 95.6767 15.10369545300601Epoch: 2025-11-02T11:40Z
TLE epoch observation values (Epoch: 2025-11-02T11:40:36.495Z)
Latitude
0.00001°
Longitude
81.64577°
Altitude
538.666 km
Speed
7.593 km/s
True Right ascension
19h 55m 11s
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
17:44:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
537.253 km
Perigee altitude
526.855 km
Semi-major axis
6,910.191 km
Eccentricity
0.00075
Inclination
97.475°
RAAN
298.7994°
Arg. of periapsis
264.3605°
True anomaly
95.76249°
Mean anomaly
95.6767°
Eccentric anomaly
95.71959°
Mean motion
3.7784 °/min
Orbital period
95.28 mins
BSTAR
0.0001778
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-11-03 22:48:22.048Z | 113.729° SE | 2025-11-03 22:50:22.048Z | 79.875° E | 19.307° | 2025-11-03 22:53:22.048Z | 23.89° NE |
| 5 mins | 2025-11-04 00:23:22.048Z | 224.071° SW | 2025-11-04 00:25:22.048Z | 270.14° WNW | 23.287° | 2025-11-04 00:28:22.048Z | 321.429° NNW |
| 5 mins | 2025-11-04 11:58:22.048Z | 53.177° ENE | 2025-11-04 12:00:22.048Z | 111.781° ESE | 28.258° | 2025-11-04 12:03:22.048Z | 162.658° S |
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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