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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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 26046.86272926 .00004144 00000-0 25056-3 0 9993
2 45602 97.4813 41.7566 0007554 261.4489 98.5885 15.11174876316515Epoch: 2026-02-15T20:42Z
TLE epoch observation values (Epoch: 2026-02-15T20:42:19.808Z)
Latitude
-0.00002°
Longitude
-54.69127°
Altitude
536.476 km
Speed
7.594 km/s
True Right ascension
02h 47m 01s
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
04:40:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
534.815 km
Perigee altitude
524.379 km
Semi-major axis
6,907.734 km
Eccentricity
0.00076
Inclination
97.4813°
RAAN
41.7566°
Arg. of periapsis
261.4489°
True anomaly
98.67408°
Mean anomaly
98.5885°
Eccentric anomaly
98.63129°
Mean motion
3.78042 °/min
Orbital period
95.23 mins
BSTAR
0.00025056
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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 | 2026-02-16 11:35:26.011Z | 50.41° ENE | 2026-02-16 11:37:26.011Z | 84.69° E | 18.819° | 2026-02-16 11:40:26.011Z | 139.996° SSE |
| 4 mins | 2026-02-16 13:10:26.011Z | 330.101° NNW | 2026-02-16 13:12:26.011Z | 284.069° WNW | 23.456° | 2026-02-16 13:14:26.011Z | 243.221° WSW |
| 6 mins | 2026-02-16 23:51:26.011Z | 186.843° SSW | 2026-02-16 23:53:26.011Z | 234.225° WSW | 39.068° | 2026-02-16 23:57:26.011Z | 339.02° 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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