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: 15 hours ago
TLE from 15 hours ago
0 OBJECT G
1 61900U 24205G 25258.52519142 .00012528 00000-0 65155-3 0 9993
2 61900 97.4450 330.4359 0025017 270.5428 89.2938 15.15919453 46627Epoch: 2025-09-15T12:36Z
TLE epoch observation values (Epoch: 2025-09-15T12:36:16.538Z)
Latitude
-0.00006°
Longitude
146.6384°
Altitude
521.103 km
Speed
7.603 km/s
True Right ascension
22h 01m 44s
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
20:43:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
532.406 km
Perigee altitude
497.917 km
Semi-major axis
6,893.299 km
Eccentricity
0.0025
Inclination
97.445°
RAAN
330.4359°
Arg. of periapsis
270.5428°
True anomaly
89.58046°
Mean anomaly
89.2938°
Eccentric anomaly
89.43713°
Mean motion
3.7923 °/min
Orbital period
94.93 mins
BSTAR
0.00065155
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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 | 2025-09-16 04:34:30.820Z | 146.234° SSE | 2025-09-16 04:37:30.820Z | 83.661° E | 36.37° | 2025-09-16 04:40:30.820Z | 4.094° NNE |
| 6 mins | 2025-09-16 17:41:30.820Z | 15.695° NNE | 2025-09-16 17:44:30.820Z | 156.607° SSE | 43.714° | 2025-09-16 17:47:30.820Z | 188.906° 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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