OBJECT G, 61900
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 G, 61900 is a satellite owned by Yunyao yuhang (CN) 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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61900 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
None
Manufacturer
Changguang WJ
Mission
Operational Commercial Weather
Bus & Motor
YY-1, Unknown motor
Mass
~50 kg wet, ~50 kg dry
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: 20 hours ago
TLE from 20 hours ago
0 OBJECT G
1 61900U 24205G 25252.32015846 .00008736 00000-0 45703-3 0 9990
2 61900 97.4460 324.3521 0025056 293.4812 66.3788 15.15810860 45681Epoch: 2025-09-09T07:41Z
TLE epoch observation values (Epoch: 2025-09-09T07:41:01.69Z)
Latitude
-0.00001°
Longitude
-139.51756°
Altitude
514.712 km
Speed
7.61 km/s
True Right ascension
21h 37m 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
19:43:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
532.764 km
Perigee altitude
498.218 km
Semi-major axis
6,893.628 km
Eccentricity
0.00251
Inclination
97.446°
RAAN
324.3521°
Arg. of periapsis
293.4812°
True anomaly
66.64219°
Mean anomaly
66.3788°
Eccentric anomaly
66.51046°
Mean motion
3.79203 °/min
Orbital period
94.94 mins
BSTAR
0.00045703
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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 G 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 | 2025-09-10 04:24:35.358Z | 137.486° SSE | 2025-09-10 04:27:35.358Z | 80.719° E | 29.922° | 2025-09-10 04:30:35.358Z | 10.942° NNE |
| 6 mins | 2025-09-10 17:31:35.358Z | 24.006° NE | 2025-09-10 17:34:35.358Z | 118.908° SE | 40.011° | 2025-09-10 17:37:35.358Z | 178.731° S |
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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