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KUIPER-P2, 58013

Orbit data source: Space-Track

KUIPER-P2, 58013 is 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). Payload-class satellites include a variety of spacecraft 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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https://www.satcat.com/sats-embedded/58013?theme=dark&initialShowStats=false

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Identifier	58013, 2023-154A
Orbit	LEO
Last TLE update	3 hours ago
Origin	AMAZ (US)
Manufacturer	Kuiper Systems
Mission	Operational Commercial Communications
Bus & Motor	KUIPER, 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 & HBR	Box + 2 Pan, 10 m
Radar Cross Section	10.304 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 3 hours ago

0 KUIPER-P2
1 58013U 23154A   25093.25002315  .00256575  00000-0  13685-2 0  9994
2 58013  29.9624   6.6909 0006536  13.0549 352.9319 15.78539602 83743

Epoch: 2025-04-03T06:00Z

Definitive object data (Epoch: 2025-04-03T06:00:02Z)

Latitude	2.9672°
Longitude	89.98655°
Altitude	328.25 km
Speed	7.717 km/s
True Right ascension	00h 47m 16s
True Declination	2° 56' 54"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	29.40479°
Longitude	160.28997°
Altitude	331.502 km
Speed	7.716 km/s
Apparent Right ascension	04h 24m 32s
Apparent Declination	-4° 26' 07"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	15:07:43
Azimuth	328.957° NNW
Elevation	-50.513°
Doppler factor	1

Orbital elements

Apogee altitude	343.08 km
Perigee altitude	334.3 km
Semi-major axis	6,716.827 km
Eccentricity	0.0006536
Inclination	29.9624°
RAAN	6.6909°
Arg. of periapsis	13.0549°
True anomaly	352.92268°
Mean anomaly	352.9319°
Eccentric anomaly	352.92729°
Mean motion	3.94273 °/min
BSTAR	0.0013685
Orbital period	91.31 mins