OBJECT A, 62081
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 A, 62081 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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62081 intel report (Beta)
OBJECT A 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 A
1 62081U 24219A 24348.75433467 .00003582 00000-0 51447-3 0 9997
2 62081 97.9486 147.4363 0001563 10.3449 349.7793 14.77071685 2736Epoch: 2024-12-13T18:06Z
Definitive object data (Epoch: 2024-12-13T18:06:14.515Z)
| Latitude | -0.00003° |
| Longitude | 152.96005° |
| Altitude | 640.519 km |
| Speed | 7.538 km/s |
| True Right ascension | 09h 49m 44s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 19.14855° |
| Longitude | 150.39994° |
| Altitude | 640.023 km |
| Speed | 7.54 km/s |
| Apparent Right ascension | 09h 38m 03s |
| Apparent Declination | -8° 47' 08" |
| Sunlit | Object is in full shadow |
Visualization observer readout
| Local Sidereal Time | 21:36:06 |
| Azimuth | 359.065° N |
| Elevation | -58.866° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 636.726 km |
| Perigee altitude | 634.533 km |
| Semi-major axis | 7,013.767 km |
| Eccentricity | 0.0001563 |
| Inclination | 97.9486° |
| RAAN | 147.4363° |
| Arg. of periapsis | 10.3449° |
| True anomaly | 349.77612° |
| Mean anomaly | 349.7793° |
| Eccentric anomaly | 349.77771° |
| Mean motion | 3.69501 °/min |
| BSTAR | 0.00051447 |
| Orbital period | 97.43 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 A 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2024-12-13 23:33:05.806Z | 17.878° NNE | 2024-12-13 23:37:05.806Z | 137.958° SSE | 43.025° | 2024-12-13 23:41:05.806Z | 186.951° SSW |
| 7 mins | 2024-12-14 10:30:05.806Z | 144.728° SSE | 2024-12-14 10:33:05.806Z | 61.456° ENE | 39.17° | 2024-12-14 10:37:05.806Z | 356.849° N |
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