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: 9 hours ago
TLE from 9 hours ago
0 XINGYUN-2 01
1 45602U 20028A 25307.81154669 .00003111 00000-0 19322-3 0 9992
2 45602 97.4749 300.0929 0007583 258.7831 101.2546 15.10378462300806Epoch: 2025-11-03T19:28Z
TLE epoch observation values (Epoch: 2025-11-03T19:28:37.634Z)
Latitude
-0.00005°
Longitude
-35.37146°
Altitude
539.147 km
Speed
7.592 km/s
True Right ascension
20h 00m 22s
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
00:30:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
537.267 km
Perigee altitude
526.787 km
Semi-major axis
6,910.164 km
Eccentricity
0.00076
Inclination
97.4749°
RAAN
300.0929°
Arg. of periapsis
258.7831°
True anomaly
101.33981°
Mean anomaly
101.2546°
Eccentric anomaly
101.29721°
Mean motion
3.77842 °/min
Orbital period
95.28 mins
BSTAR
0.00019322
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-11-04 11:56:41.132Z | 33.28° NE | 2025-11-04 11:59:41.132Z | 88.329° E | 28.632° | 2025-11-04 12:02:41.132Z | 157.163° SSE |
| 5 mins | 2025-11-05 00:14:41.132Z | 220.567° SW | 2025-11-05 00:16:41.132Z | 278.752° WNW | 27.567° | 2025-11-05 00:19:41.132Z | 327.762° NNW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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