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). 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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58014 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: 1 year ago
TLE from 1 year 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
TLE epoch observation values (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
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
01:00:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
191.352 km
Perigee altitude
190.745 km
Semi-major axis
6,569.185 km
Eccentricity
0.00005
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
Orbital period
88.31 mins
BSTAR
0.0020153
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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-P1 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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