OBJECT J, 61902
Orbit data source: Space-Track
You're viewing an Uncataloged Satellite
Recently launched and/or uncataloged satellites may have evolving metadata. Metadata may include but not limited to: Owner, Maufacturer, Bus, Motor, and Mission.
OBJECT J, 61902 is a Chinese satellite in SSO that was launched on Mon, 11 Nov 2024 UTC via a LIJIAN-1 launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). Unknown objects in Earth's orbit typically refer to objects detected orbiting the Earth but have not yet been identified or cataloged. These objects could be anything from previously untracked satellites, spent rocket stages, debris from satellite collisions, or even natural meteoroids temporarily captured by Earth's gravity.
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61902 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
None
Manufacturer
Unknown
Mission
Operational Commercial Meteo Radio Occ.
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box + 1 Pan, 2.5 m
Radar Cross Section
5.339 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 OBJECT J
1 61902U 24205J 26032.73918448 .00000253 00000-0 19186-4 0 9997
2 61902 97.4287 107.1569 0012902 271.0529 88.9222 15.10329055 67731Epoch: 2026-02-01T17:44Z
TLE epoch observation values (Epoch: 2026-02-01T17:44:25.539Z)
Latitude
-0.00006°
Longitude
69.10599°
Altitude
538.116 km
Speed
7.594 km/s
True Right ascension
07h 08m 37s
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
04:48:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
541.091 km
Perigee altitude
523.26 km
Semi-major axis
6,910.312 km
Eccentricity
0.00129
Inclination
97.4287°
RAAN
107.1569°
Arg. of periapsis
271.0529°
True anomaly
89.07002°
Mean anomaly
88.9222°
Eccentric anomaly
88.99611°
Mean motion
3.7783 °/min
Orbital period
95.28 mins
BSTAR
0.000019186
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Other satellites on launch #205 in the year 2024 (2024-11-11 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.OBJECT J 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-02-04 04:41:38.272Z | 156.544° SSE | 2026-02-04 04:45:38.272Z | 34.746° NE | 40.34° | 2026-02-04 04:48:38.272Z | 355.078° N |
| 5 mins | 2026-02-04 17:52:38.272Z | 1.332° NNE | 2026-02-04 17:54:38.272Z | 272.682° WNW | 43.217° | 2026-02-04 17:57:38.272Z | 201.952° SSW |
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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