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 | 15 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 15 hours ago
0 OBJECT E
1 61898U 24205E 24348.31154442 .00015100 00000-0 79319-3 0 9999
2 61898 97.4727 59.9452 0014678 167.3861 192.7742 15.15702820 4830Epoch: 2024-12-13T07:28Z
Definitive object data (Epoch: 2024-12-13T07:28:37.437Z)
| Latitude | -0.00003° |
| Longitude | -134.69012° |
| Altitude | 531.804 km |
| Speed | 7.591 km/s |
| True Right ascension | 03h 59m 46s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | 82.27649° |
| Longitude | 151.79001° |
| Altitude | 530.103 km |
| Speed | 7.606 km/s |
| Apparent Right ascension | 08h 08m 47s |
| Apparent Declination | 33° 19' 11" |
| Sunlit | Object is in partial shadow |
Visualization observer readout
| Local Sidereal Time | 20:39:16 |
| Azimuth | 6.633° NNE |
| Elevation | -16.426° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 525.939 km |
| Perigee altitude | 505.701 km |
| Semi-major axis | 6,893.957 km |
| Eccentricity | 0.0014678 |
| Inclination | 97.4727° |
| RAAN | 59.9452° |
| Arg. of periapsis | 167.3861° |
| True anomaly | 192.73708° |
| Mean anomaly | 192.7742° |
| Eccentric anomaly | 192.75563° |
| Mean motion | 3.79176 °/min |
| BSTAR | 0.00079319 |
| Orbital period | 94.94 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2024-12-14 04:13:25.190Z | 114.546° SE | 2024-12-14 04:15:25.190Z | 79.027° E | 19.883° | 2024-12-14 04:18:25.190Z | 22.106° NNE |
| 4 mins | 2024-12-14 05:48:25.190Z | 232.102° WSW | 2024-12-14 05:49:25.190Z | 254.259° W | 21.596° | 2024-12-14 05:52:25.190Z | 314.473° NW |
| 5 mins | 2024-12-14 17:20:25.190Z | 51.102° ENE | 2024-12-14 17:22:25.190Z | 107.329° ESE | 27.326° | 2024-12-14 17:25:25.190Z | 161.436° S |
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