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: 11 hours ago
TLE from 11 hours ago
0 XINGYUN-2 01
1 45602U 20028A 25261.29769988 .00002161 00000-0 13686-3 0 9990
2 45602 97.4723 254.7025 0011279 65.0149 295.2251 15.09961962293784Epoch: 2025-09-18T07:08Z
TLE epoch observation values (Epoch: 2025-09-18T07:08:41.269Z)
Latitude
-0.00001°
Longitude
150.06924°
Altitude
536.074 km
Speed
7.596 km/s
True Right ascension
16h 58m 48s
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
10:43:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
541.094 km
Perigee altitude
525.503 km
Semi-major axis
6,911.435 km
Eccentricity
0.00113
Inclination
97.4723°
RAAN
254.7025°
Arg. of periapsis
65.0149°
True anomaly
295.10811°
Mean anomaly
295.2251°
Eccentric anomaly
295.16661°
Mean motion
3.77738 °/min
Orbital period
95.3 mins
BSTAR
0.00013686
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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 | 2025-09-18 23:10:56.633Z | 136.512° SSE | 2025-09-18 23:13:56.633Z | 74.46° E | 30.418° | 2025-09-18 23:16:56.633Z | 9.379° NNE |
| 6 mins | 2025-09-19 12:20:56.633Z | 22.961° NE | 2025-09-19 12:22:56.633Z | 60.565° ENE | 40.225° | 2025-09-19 12:26:56.633Z | 182.604° SSW |
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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