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, 0.3 m
Radar Cross Section
0.569 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 XINGYUN-2 01
1 45602U 20028A 26252.58889094 .00002372 00000-0 14139-3 0 9992
2 45602 97.4936 243.3651 0007432 276.7201 83.3184 15.12115746347590Epoch: 2026-09-09T14:08Z
TLE epoch observation values (Epoch: 2026-09-09T14:08:00.177Z)
Latitude
0.00002°
Longitude
42.72557°
Altitude
532.232 km
Speed
7.597 km/s
True Right ascension
16h 13m 27s
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
15:53:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
531.861 km
Perigee altitude
521.597 km
Semi-major axis
6,904.866 km
Eccentricity
0.00074
Inclination
97.4936°
RAAN
243.3651°
Arg. of periapsis
276.7201°
True anomaly
83.403°
Mean anomaly
83.3184°
Eccentric anomaly
83.3607°
Mean motion
3.78277 °/min
Orbital period
95.17 mins
BSTAR
0.00014139
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-09-09 23:46:56.145Z | 182.899° SSW | 2026-09-09 23:49:56.145Z | 240.752° WSW | 53.664° | 2026-09-09 23:53:56.145Z | 338.69° N |
| 5 mins | 2026-09-10 12:56:56.145Z | 333.177° NNW | 2026-09-10 12:58:56.145Z | 277.347° WNW | 32.216° | 2026-09-10 13:01:56.145Z | 224.924° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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