OBJECT G, 61900
Orbit data source: Space-Track
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.
61900 intel report (Beta)
OBJECT G details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 9 hours ago |
| Origin | |
| Manufacturer | Yunyao yuhang |
| Mission | Operational spacecraft |
| 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 | Unknown |
| Radar Cross Section | Medium (>0.1 m² and <1 m²) |
Expand to show TLE details & history
TLE from 9 hours ago
0 OBJECT G
1 61900U 24205G 24348.57480012 .00016312 00000-0 85573-3 0 9991
2 61900 97.4742 60.2122 0014322 167.5018 192.6573 15.15738308 4877Definitive object data (Epoch: 2024-12-13T13:47:42.73Z)
| Latitude | 0.00002° |
| Longitude | 130.54534° |
| Altitude | 531.461 km |
| Speed | 7.592 km/s |
| True Right ascension | 04h 00m 50s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | -52.88965° |
| Longitude | 140.85611° |
| Altitude | 546.902 km |
| Speed | 7.583 km/s |
| Apparent Right ascension | 07h 22m 25s |
| Apparent Declination | -52° 41' 18" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 21:35:57 |
| Azimuth | 130.538° SE |
| Elevation | -63.967° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 525.586 km |
| Perigee altitude | 505.839 km |
| Semi-major axis | 6,893.849 km |
| Eccentricity | 0.0014322 |
| Inclination | 97.4742° |
| RAAN | 60.2122° |
| Arg. of periapsis | 167.5018° |
| True anomaly | 192.6214° |
| Mean anomaly | 192.6573° |
| Eccentric anomaly | 192.63934° |
| Mean motion | 3.79184 °/min |
| BSTAR | 0.00085573 |
| Orbital period | 94.94 mins |
Other satellites on launch #205 in the year 2024 (2024-11-11 UTC)
OBJECT G Visibility forecast
Observer location: undefined°, undefined
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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2024-12-14 04:11:56.997Z | 117.061° SE | 2024-12-14 04:14:56.997Z | 62.389° ENE | 19.504° | 2024-12-14 04:16:56.997Z | 26.095° NE |
| 4 mins | 2024-12-14 05:46:56.997Z | 226.138° WSW | 2024-12-14 05:48:56.997Z | 272.632° WNW | 22.304° | 2024-12-14 05:50:56.997Z | 311.687° NW |
| 5 mins | 2024-12-14 17:18:56.997Z | 47.644° ENE | 2024-12-14 17:20:56.997Z | 97.753° ESE | 26.897° | 2024-12-14 17:23:56.997Z | 158.233° S |
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