XINGYUN-2 02, 45603
Orbit data source: Space-Track
XINGYUN-2 02, 45603 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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45603 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, 0.3 m
Radar Cross Section
0.569 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 XINGYUN-2 02
1 45603U 20028B 26252.58319319 .00001297 00000-0 79612-4 0 9994
2 45603 97.5111 257.1227 0010730 351.3646 8.7398 15.11822307347581Epoch: 2026-09-09T13:59Z
TLE epoch observation values (Epoch: 2026-09-09T13:59:47.891Z)
Latitude
-0.00004°
Longitude
58.53999°
Altitude
526.39 km
Speed
7.604 km/s
True Right ascension
17h 08m 29s
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
15:54:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
535.034 km
Perigee altitude
520.214 km
Semi-major axis
6,905.761 km
Eccentricity
0.00107
Inclination
97.5111°
RAAN
257.1227°
Arg. of periapsis
351.3646°
True anomaly
8.75851°
Mean anomaly
8.7398°
Eccentric anomaly
8.74915°
Mean motion
3.78204 °/min
Orbital period
95.19 mins
BSTAR
0.000079612
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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 02 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-09 23:40:24.006Z | 118.073° SE | 2026-09-09 23:43:24.006Z | 57.83° ENE | 23.004° | 2026-09-09 23:45:24.006Z | 22.123° NNE |
| 4 mins | 2026-09-10 01:15:24.006Z | 227.824° WSW | 2026-09-10 01:17:24.006Z | 269.948° W | 21.848° | 2026-09-10 01:19:24.006Z | 308.062° NW |
| 5 mins | 2026-09-10 12:49:24.006Z | 43.745° NE | 2026-09-10 12:51:24.006Z | 100.233° ESE | 38.242° | 2026-09-10 12:54:24.006Z | 164.024° S |
| 4 mins | 2026-09-10 23:31:24.006Z | 94.369° ESE | 2026-09-10 23:32:24.006Z | 75.355° E | 18.106° | 2026-09-10 23:35:24.006Z | 23.941° NE |
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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