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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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: 9 hours ago
TLE from 9 hours ago
0 XINGYUN-2 02
1 45603U 20028B 25307.82267087 .00003210 00000-0 20011-3 0 9990
2 45603 97.5102 312.9713 0010428 335.4708 24.6024 15.10209331300809Epoch: 2025-11-03T19:44Z
TLE epoch observation values (Epoch: 2025-11-03T19:44:38.763Z)
Latitude
-0.00001°
Longitude
-26.50874°
Altitude
532.08 km
Speed
7.6 km/s
True Right ascension
20h 51m 53s
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
00:30:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
539.751 km
Perigee altitude
525.338 km
Semi-major axis
6,910.681 km
Eccentricity
0.00104
Inclination
97.5102°
RAAN
312.9713°
Arg. of periapsis
335.4708°
True anomaly
24.65221°
Mean anomaly
24.6024°
Eccentric anomaly
24.6273°
Mean motion
3.778 °/min
Orbital period
95.29 mins
BSTAR
0.00020011
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-11-04 13:48:13.024Z | 350.081° N | 2025-11-04 13:51:13.024Z | 269.777° W | 32.387° | 2025-11-04 13:54:13.024Z | 218.013° SW |
| 6 mins | 2025-11-05 00:30:13.024Z | 165.569° S | 2025-11-05 00:32:13.024Z | 160.666° S | 42.68° | 2025-11-05 00:36:13.024Z | 348.662° N |
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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