XJS G, 45611 (Decayed)
Orbit data source: Space-Track
XJS G, 45611 was a payload satellite owned by SECM (CN) in LEO that was launched on Fri, 29 May 2020 UTC via a CHANG ZHENG 11 launch vehicle from the Xichang Space Center, China (XSC). 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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45611 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SECM
Mission
Decayed Civil Technology
Bus & Motor
CX6, Unknown motor
Mass
~20 kg wet, ~20 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, Unknown HBR
Radar Cross Section
0.080 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 months ago
TLE from 11 months ago
0 XJS G
1 45611U 20032A 25218.61004394 .05589139 13794-5 52431-3 0 9996
2 45611 35.0147 187.6493 0003705 241.9551 118.0825 16.37523590292198Epoch: 2025-08-06T14:38Z
TLE epoch observation values (Epoch: 2025-08-06T14:38:27.796Z)
Latitude
-0°
Longitude
12.64714°
Altitude
172.396 km
Speed
7.805 km/s
True Right ascension
12h 30m 35s
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
21:33:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
178.235 km
Perigee altitude
173.379 km
Semi-major axis
6,553.944 km
Eccentricity
0.00037
Inclination
35.0147°
RAAN
187.6493°
Arg. of periapsis
241.9551°
True anomaly
118.11995°
Mean anomaly
118.0825°
Eccentric anomaly
118.10123°
Mean motion
4.09062 °/min
Orbital period
88.01 mins
BSTAR
0.00052431
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Other satellites on launch #32 in the year 2020 (2020-05-29 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.XJS G Visibility
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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. |
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| This satellite is decayed. |
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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