OBJECT K, 58471
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 K, 58471 is a satellite in SSO that was launched on Fri, 01 Dec 2023 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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58471 intel report (Beta)
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OBJECT K radio frequencies
OBJECT K details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 5 hours ago |
| Origin | |
| Manufacturer | NPUA/BAZMQ |
| Mission | Operational Amateur Technology |
| Bus & Motor | CUBESAT 1U, Unknown motor |
| Mass | 1 kg wet, 1 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Unknown |
| Shape & HBR | Box, 0.1 m |
| Radar Cross Section | 0.015 m², Small (<0.1 m²) |
Expand to show TLE details & history
TLE from 5 hours ago
0 OBJECT K
1 58471U 23185K 25003.13545637 .00099599 00000-0 18142-2 0 9997
2 58471 97.3957 77.0665 0006976 282.0471 77.9998 15.49098328 60824Epoch: 2025-01-03T03:15Z
Definitive object data (Epoch: 2025-01-03T03:15:03.43Z)
| Latitude | -0.00001° |
| Longitude | -74.70216° |
| Altitude | 421.509 km |
| Speed | 7.659 km/s |
| True Right ascension | 05h 08m 15s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | -5.05062° |
| Longitude | 104.87675° |
| Altitude | 423.671 km |
| Speed | 7.656 km/s |
| Apparent Right ascension | 18h 32m 33s |
| Apparent Declination | -23° 54' 12" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 08:34:20 |
| Azimuth | 67.178° ENE |
| Elevation | -59.826° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 421.029 km |
| Perigee altitude | 411.549 km |
| Semi-major axis | 6,794.426 km |
| Eccentricity | 0.0006976 |
| Inclination | 97.3957° |
| RAAN | 77.0665° |
| Arg. of periapsis | 282.0471° |
| True anomaly | 78.07801° |
| Mean anomaly | 77.9998° |
| Eccentric anomaly | 78.0389° |
| Mean motion | 3.87538 °/min |
| BSTAR | 0.0018142 |
| Orbital period | 92.89 mins |
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Other satellites on launch #185 in the year 2023 (2023-12-01 UTC)
OBJECT K 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 | 2025-01-03 17:45:54.009Z | 5.361° NNE | 2025-01-03 17:47:54.009Z | 327.756° NNW | 41.974° | 2025-01-03 17:50:54.009Z | 200.47° SSW |
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