KUIPER-P2, 58013 (Decayed)
Orbit data source: Space-Track
KUIPER-P2, 58013 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). 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.
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58013 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
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
Shape & HBR
Box + 2 Pan, 5.0 m
Radar Cross Section
10.304 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 5 months ago
TLE from 5 months ago
0 KUIPER-P2
1 58013U 23154A 25118.58335648 .00468493 82989-4 98019-3 0 9995
2 58013 29.9535 181.0087 0003053 52.3598 284.3262 15.97756228 87778Epoch: 2025-04-28T14:00Z
TLE epoch observation values (Epoch: 2025-04-28T14:00:01.999Z)
Latitude
-11.50644°
Longitude
93.64125°
Altitude
280.687 km
Speed
7.741 km/s
True Right ascension
10h 41m 46s
True Declination
-11° 26' 05"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
02:55:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
286.826 km
Perigee altitude
282.758 km
Semi-major axis
6,662.929 km
Eccentricity
0.00031
Inclination
29.9535°
RAAN
181.0087°
Arg. of periapsis
52.3598°
True anomaly
284.2923°
Mean anomaly
284.3262°
Eccentric anomaly
284.30925°
Mean motion
3.99067 °/min
Orbital period
90.21 mins
BSTAR
0.00098019
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Other satellites on launch #154 in the year 2023 (2023-10-06 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.KUIPER-P2 Visibility
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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. |
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| This satellite is decayed. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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