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 26136.89983373 .00001319 00000-0 81288-4 0 9992
2 45602 97.4861 129.9253 0007970 322.2349 37.8321 15.11666029330112Epoch: 2026-05-16T21:35Z
TLE epoch observation values (Epoch: 2026-05-16T21:35:45.634Z)
Latitude
-0.00003°
Longitude
-68.62501°
Altitude
529.847 km
Speed
7.6 km/s
True Right ascension
08h 39m 42s
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
10:56:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
533.603 km
Perigee altitude
522.595 km
Semi-major axis
6,906.236 km
Eccentricity
0.0008
Inclination
97.4861°
RAAN
129.9253°
Arg. of periapsis
322.2349°
True anomaly
37.88816°
Mean anomaly
37.8321°
Eccentric anomaly
37.86013°
Mean motion
3.78165 °/min
Orbital period
95.2 mins
BSTAR
0.000081288
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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 | 2026-05-17 12:27:25.182Z | 9.395° NNE | 2026-05-17 12:30:25.182Z | 320.415° NNW | 44.465° | 2026-05-17 12:33:25.182Z | 197.204° SSW |
| 6 mins | 2026-05-17 23:09:25.182Z | 136.513° SSE | 2026-05-17 23:11:25.182Z | 91.78° ESE | 33.093° | 2026-05-17 23:15:25.182Z | 2.342° NNE |
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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