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DECAYED
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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.

Not visible in the next 10 days
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KUIPER-P1 details
Identifier
58014, 2023-154B
Orbit
Decayed
Last TLE update1 month ago
Origin
Flag of USKuiper Systems (US)
ManufacturerKuiper Systems
MissionDecayed Commercial Communications
Bus & MotorKUIPER, Unknown motor
Mass~600 kg wet, ~600 kg dry
Launch date (UTC)
2023-10-06 (1 year ago)
Launch vehicle
ATLAS V 501
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBRBox + 2 Pan, 10 m
Radar Cross Section10.304 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 1 month 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 55224
Epoch: 2024-09-28T20:33Z
Definitive object data (Epoch: 2024-09-28T20:33:23.776Z)
Latitude26.9335°
Longitude-79.78286°
Altitude185.774 km
Speed7.8 km/s
True Right ascension15h 46m 41s
True Declination26° 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
Apogee191.352 km
Perigee190.745 km
Semi-major axis6,569.185 km
Eccentricity0.0000462
Inclination29.9543°
RAAN175.4443°
Arg. of periapsis256.428°
True anomaly168.15179°
Mean anomaly168.1507°
Eccentric anomaly168.15124°
Mean motion4.07639 °/min
BSTAR0.0020153
Period88.31 mins
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Other satellites on launch #154 in the year 2023 (2023-10-06 UTC)

KUIPER-P1 Visibility forecast

Observer location: undefined°, undefined

This satellite is decayed
Span
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Start Az.
Max El. time (UTC)
Max El. Az.
Max El.
End time (UTC)
End Az.
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