OBJECT G, 61443 (Decayed)
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, 61443 was a satellite owned by CASC (CN) in LEO that was launched on Tue, 24 Sep 2024 UTC launched 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. This object's orbit decayed before it could be identified.
61443 intel report (Beta)
OBJECT G details
| Identifier | |
| Orbit | Decayed |
| Last TLE update | 1 month ago |
| Origin | |
| Manufacturer | CAS |
| Mission | Decayed spacecraft |
| Bus & Motor | Unknown |
| Mass | Unknown |
| Launch date (UTC) | |
| Launch vehicle | Unknown |
| Launch site | |
| Object type | Unknown |
| Shape & HBR | Unknown |
| Radar Cross Section | RCS unknown |
Expand to show TLE details & history
TLE from 1 month ago
0 OBJECT G
1 61443U 24174G 24311.05781089 .11536702 23229-5 77814-3 0 9993
2 61443 97.4009 319.3428 0032307 235.3272 124.4980 16.37015076 6390Definitive object data (Epoch: 2024-11-06T01:23:14.86Z)
| Latitude | -0.00009° |
| Longitude | -107.2294° |
| Altitude | 189.04 km |
| Speed | 7.786 km/s |
| True Right ascension | 21h 17m 22s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization observer readout
| Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed. |
Visualization observer readout
| Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed. |
Orbital elements
| Apogee altitude | 191.723 km |
| Perigee altitude | 149.409 km |
| Semi-major axis | 6,548.703 km |
| Eccentricity | 0.0032307 |
| Inclination | 97.4009° |
| RAAN | 319.3428° |
| Arg. of periapsis | 235.3272° |
| True anomaly | 124.80241° |
| Mean anomaly | 124.498° |
| Eccentric anomaly | 124.65027° |
| Mean motion | 4.09553 °/min |
| BSTAR | 0.00077814 |
| Orbital period | 87.9 mins |
Other satellites on launch #174 in the year 2024 (2024-09-24 UTC)
| OBJECT A, 61238 |
| OBJECT B, 61239 |
| OBJECT C, 61240 |
| OBJECT D, 61241 |
| OBJECT E, 61242 |
| OBJECT F, 61263 |
| OBJECT G, 61443 (Decayed) |
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. |
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