KUIPER-P1, 58014 (Decayed)
Orbit data source: Space-Track
KUIPER-P1, 58014 was a payload satellite owned by Kuiper Systems (US) in LEO that was launched on Fri, 06 Oct 2023 UTC via an ATLAS V 501 launch vehicle from the Air Force Eastern Test Range (AFETR). Payloads include a variety of satellites, spacecraft, and rockets equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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58014 intel report (Beta)
KUIPER-P1 details
| Identifier | |
| Orbit | Decayed |
| Last TLE update | 3 months ago |
| Origin | |
| Manufacturer | Kuiper Systems |
| Mission | Decayed Commercial Communications |
| Bus & Motor | KUIPER, Unknown motor |
| Mass | ~600 kg wet, ~600 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Box + 2 Pan, 10 m |
| Radar Cross Section | 10.304 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 3 months ago
0 KUIPER-P1
1 58014U 23154B 24272.85652519 .12081399 -54635-5 20153-2 0 9996
2 58014 29.9543 175.4443 0000462 256.4280 168.1507 16.32122349 55224Epoch: 2024-09-28T20:33Z
Definitive object data (Epoch: 2024-09-28T20:33:23.776Z)
| Latitude | 26.9335° |
| Longitude | -79.78286° |
| Altitude | 185.774 km |
| Speed | 7.8 km/s |
| True Right ascension | 15h 46m 41s |
| True Declination | 26° 46' 58" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization observer readout
| Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed. |
Visualization observer readout
| Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed. |
Orbital elements
| Apogee altitude | 191.352 km |
| Perigee altitude | 190.745 km |
| Semi-major axis | 6,569.185 km |
| Eccentricity | 0.0000462 |
| Inclination | 29.9543° |
| RAAN | 175.4443° |
| Arg. of periapsis | 256.428° |
| True anomaly | 168.15179° |
| Mean anomaly | 168.1507° |
| Eccentric anomaly | 168.15124° |
| Mean motion | 4.07639 °/min |
| BSTAR | 0.0020153 |
| Orbital period | 88.31 mins |
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Other satellites on launch #154 in the year 2023 (2023-10-06 UTC)
| KUIPER-P2, 58013 |
| KUIPER-P1, 58014 (Decayed) |
| ATLAS 5 CENTAUR R/B, 58015 |
KUIPER-P1 Visibility forecast
Observer location: undefined°, undefined
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