OBJECT E, 62085
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, 62085 is a satellite in SSO that was launched on Mon, 25 Nov 2024 UTC via an ELECTRON launch vehicle from the Rocket Lab Launch Complex (RLLC). 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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62085 intel report (Beta)
OBJECT E details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 5 hours ago |
| Origin | |
| Manufacturer | KINEIS |
| Mission | Operational spacecraft |
| Bus & Motor | CUBESAT 16U, Unknown motor |
| Mass | 28 kg wet, 28 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 62085U 24219E 24348.74696483 .00001560 00000-0 22524-3 0 9997
2 62085 97.9499 147.4459 0001247 223.0236 137.0877 14.77632841 2734Epoch: 2024-12-13T17:55Z
Definitive object data (Epoch: 2024-12-13T17:55:37.761Z)
| Latitude | -0.00003° |
| Longitude | 155.63005° |
| Altitude | 640.464 km |
| Speed | 7.537 km/s |
| True Right ascension | 09h 49m 47s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 53.6006° |
| Longitude | 144.98131° |
| Altitude | 646.463 km |
| Speed | 7.539 km/s |
| Apparent Right ascension | 09h 22m 06s |
| Apparent Declination | 9° 46' 14" |
| Sunlit | Object is in full shadow |
Visualization observer readout
| Local Sidereal Time | 21:34:50 |
| Azimuth | 4.107° NNE |
| Elevation | -40.226° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 634.727 km |
| Perigee altitude | 632.978 km |
| Semi-major axis | 7,011.989 km |
| Eccentricity | 0.0001247 |
| Inclination | 97.9499° |
| RAAN | 147.4459° |
| Arg. of periapsis | 223.0236° |
| True anomaly | 137.09743° |
| Mean anomaly | 137.0877° |
| Eccentric anomaly | 137.09256° |
| Mean motion | 3.69642 °/min |
| BSTAR | 0.00022524 |
| Orbital period | 97.39 mins |
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Other satellites on launch #219 in the year 2024 (2024-11-25 UTC)
| OBJECT A, 62081 |
| OBJECT B, 62082 |
| OBJECT C, 62083 |
| OBJECT D, 62084 |
| OBJECT E, 62085 |
| ELECTRON KICK STAGE R/B, 62086 |
| ELECTRON R/B, 62087 (Decayed) |
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 | 2024-12-13 23:22:49.985Z | 25.84° NE | 2024-12-13 23:25:49.985Z | 81.624° E | 38.562° | 2024-12-13 23:29:49.985Z | 176.112° S |
| 6 mins | 2024-12-14 10:19:49.985Z | 128.283° SE | 2024-12-14 10:21:49.985Z | 81.248° E | 33.375° | 2024-12-14 10:25:49.985Z | 3.786° NNE |
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