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 25351.59768132 .00002417 00000-0 14946-3 0 9997
2 45602 97.4756 342.8503 0010753 105.6639 254.5778 15.10733388307410Epoch: 2025-12-17T14:20Z
TLE epoch observation values (Epoch: 2025-12-17T14:20:39.666Z)
Latitude
-0.00001°
Longitude
41.21977°
Altitude
539.022 km
Speed
7.592 km/s
True Right ascension
22h 51m 24s
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
00:34:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
538.373 km
Perigee altitude
523.514 km
Semi-major axis
6,909.08 km
Eccentricity
0.00108
Inclination
97.4756°
RAAN
342.8503°
Arg. of periapsis
105.6639°
True anomaly
254.45906°
Mean anomaly
254.5778°
Eccentric anomaly
254.51843°
Mean motion
3.77931 °/min
Orbital period
95.26 mins
BSTAR
0.00014946
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-12-18 11:35:47.218Z | 55.381° ENE | 2025-12-18 11:37:47.218Z | 91.88° ESE | 18.05° | 2025-12-18 11:39:47.218Z | 130.009° SE |
| 4 mins | 2025-12-18 13:10:47.218Z | 326.308° NNW | 2025-12-18 13:12:47.218Z | 275.726° WNW | 23.649° | 2025-12-18 13:14:47.218Z | 238.207° WSW |
| 6 mins | 2025-12-18 23:51:47.218Z | 184.922° SSW | 2025-12-18 23:53:47.218Z | 233.183° WSW | 39.997° | 2025-12-18 23:57:47.218Z | 340.117° 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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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