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, 0.4 m
Radar Cross Section
0.569 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 4 hours ago
TLE from 4 hours ago
0 XINGYUN-2 01
1 45602U 20028A 26316.90589279 .00003203 00000-0 18826-3 0 9992
2 45602 97.4998 306.5211 0010547 56.7201 303.5039 15.12348313357314Epoch: 2026-11-12T21:44Z
TLE epoch observation values (Epoch: 2026-11-12T21:44:29.137Z)
Latitude
0.00004°
Longitude
-71.63298°
Altitude
528.101 km
Speed
7.601 km/s
True Right ascension
20h 26m 05s
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
21:58:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
533.302 km
Perigee altitude
518.739 km
Semi-major axis
6,904.158 km
Eccentricity
0.00105
Inclination
97.4998°
RAAN
306.5211°
Arg. of periapsis
56.7201°
True anomaly
303.40305°
Mean anomaly
303.5039°
Eccentric anomaly
303.45348°
Mean motion
3.78336 °/min
Orbital period
95.15 mins
BSTAR
0.00018826
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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 | 2026-11-13 12:35:25.894Z | 1.759° NNE | 2026-11-13 12:38:25.894Z | 303.848° NW | 55.3° | 2026-11-13 12:42:25.894Z | 206.61° SW |
| 5 mins | 2026-11-13 23:17:25.894Z | 148.324° SSE | 2026-11-13 23:19:25.894Z | 94.573° ESE | 57.776° | 2026-11-13 23:22:25.894Z | 359.162° 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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