OBJECT L, 61904
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 L, 61904 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.
61904 intel report (Beta)
OBJECT L details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 4 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 4 hours ago
0 OBJECT L
1 61904U 24205L 24326.19236170 .00019287 00000-0 10359-2 0 9996
2 61904 97.4743 38.2003 0013904 248.4986 136.4638 15.14874014 1489Definitive object data (Epoch: 2024-11-21T04:37:00.05Z)
| Latitude | 24.87385° |
| Longitude | -95.19562° |
| Altitude | 531.475 km |
| Speed | 7.595 km/s |
| True Right ascension | 02h 18m 55s |
| True Declination | 24° 44' 19" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | -59.19798° |
| Longitude | 75.79907° |
| Altitude | 534.742 km |
| Speed | 7.599 km/s |
| Apparent Right ascension | 16h 06m 26s |
| Apparent Declination | -53° 47' 36" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 05:46:55 |
| Azimuth | 137.711° SSE |
| Elevation | -68.119° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 527.926 km |
| Perigee altitude | 508.748 km |
| Semi-major axis | 6,896.474 km |
| Eccentricity | 0.0013904 |
| Inclination | 97.4743° |
| RAAN | 38.2003° |
| Arg. of periapsis | 248.4986° |
| True anomaly | 136.57341° |
| Mean anomaly | 136.4638° |
| Eccentric anomaly | 136.51862° |
| Mean motion | 3.78968 °/min |
| BSTAR | 0.0010359 |
| Orbital period | 94.99 mins |
Other satellites on launch #205 in the year 2024 (2024-11-11 UTC)
OBJECT L 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2024-11-21 17:45:00.383Z | 16.949° NNE | 2024-11-21 17:48:00.383Z | 56.923° ENE | 42.361° | 2024-11-21 17:52:00.383Z | 186.359° SSW |
| 5 mins | 2024-11-22 04:26:00.383Z | 123.004° SE | 2024-11-22 04:28:00.383Z | 80.533° E | 26.231° | 2024-11-22 04:31:00.383Z | 15.315° NNE |
| 4 mins | 2024-11-22 06:01:00.383Z | 238.596° WSW | 2024-11-22 06:02:00.383Z | 256.607° W | 16.2° | 2024-11-22 06:05:00.383Z | 308.273° NW |
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