OBJECT E, 61898
Orbit data source: Space-Track
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Recently launched and/or uncataloged satellites may have evolving metadata. Metadata may include but not limited to: Owner, Maufacturer, Bus, Motor, and Mission.
OBJECT E, 61898 is a Chinese satellite 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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61898 intel report (Beta)
OBJECT E details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 5 hours ago |
| Origin | |
| Manufacturer | Changguang WJ |
| Mission | Operational spacecraft |
| Bus & Motor | JL-1, Unknown motor |
| Mass | 42 kg wet, 42 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 5 hours ago
0 OBJECT E
1 61898U 24205E 24326.18896247 .00018992 00000-0 10254-2 0 9990
2 61898 97.4735 38.1928 0013555 246.0398 113.9414 15.14695161 1486Epoch: 2024-11-21T04:32Z
Definitive object data (Epoch: 2024-11-21T04:32:06.357Z)
| Latitude | -0.00012° |
| Longitude | -90.50795° |
| Altitude | 528.792 km |
| Speed | 7.596 km/s |
| True Right ascension | 02h 32m 46s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | -6.72392° |
| Longitude | -89.43317° |
| Altitude | 528.964 km |
| Speed | 7.596 km/s |
| Apparent Right ascension | 23h 38m 22s |
| Apparent Declination | -40° 21' 33" |
| Sunlit | Object is in full shadow |
Visualization observer readout
| Local Sidereal Time | 06:18:42 |
| Azimuth | 241.281° WSW |
| Elevation | -31.189° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 528.229 km |
| Perigee altitude | 509.531 km |
| Semi-major axis | 6,897.017 km |
| Eccentricity | 0.0013555 |
| Inclination | 97.4735° |
| RAAN | 38.1928° |
| Arg. of periapsis | 246.0398° |
| True anomaly | 114.08327° |
| Mean anomaly | 113.9414° |
| Eccentric anomaly | 114.01234° |
| Mean motion | 3.78923 °/min |
| BSTAR | 0.0010254 |
| Orbital period | 95.01 mins |
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Other satellites on launch #205 in the year 2024 (2024-11-11 UTC)
OBJECT E 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 17:46:42.593Z | 15.619° NNE | 2024-11-21 17:49:42.593Z | 43.938° NE | 42.324° | 2024-11-21 17:53:42.593Z | 187.909° SSW |
| 4 mins | 2024-11-22 04:28:42.593Z | 111.441° ESE | 2024-11-22 04:29:42.593Z | 85.87° E | 26.922° | 2024-11-22 04:32:42.593Z | 15.74° NNE |
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