KUIPER-00132, 65763
Orbit data source: Space-Track
KUIPER-00132, 65763 is a payload satellite owned by Kuiper Systems (US) in LEO that was launched on Thu, 25 Sep 2025 UTC via an ATLAS V 551 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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Identifier
Orbit
Country
USRelated business
Manufacturer
Kuiper Systems
Mission
Operational Commercial Communications
Bus & Motor
KUIPER, Unknown motor
Mass
~490 kg wet, ~490 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 3.4 m
Radar Cross Section
2.326 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 KUIPER-00132
1 65763U 25217B 26171.38472856 .00020568 00000-0 47144-3 0 9998
2 65763 51.8540 223.7452 0006918 335.6942 24.3720 15.42705454 41261Epoch: 2026-06-20T09:14Z
TLE epoch observation values (Epoch: 2026-06-20T09:14:00.547Z)
Latitude
0.00001°
Longitude
176.64281°
Altitude
434.596 km
Speed
7.655 km/s
True Right ascension
14h 54m 58s
True Declination
0° 00' 00"
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
07:16:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
443.315 km
Perigee altitude
433.884 km
Semi-major axis
6,816.737 km
Eccentricity
0.00069
Inclination
51.854°
RAAN
223.7452°
Arg. of periapsis
335.6942°
True anomaly
24.40474°
Mean anomaly
24.372°
Eccentric anomaly
24.38837°
Mean motion
3.85637 °/min
Orbital period
93.35 mins
BSTAR
0.00047144
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Other satellites on launch #217 in the year 2025 (2025-09-25 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-00132 Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-21 05:36:39.595Z | 192.359° SSW | 2026-06-21 05:38:39.595Z | 150.117° SSE | 26.444° | 2026-06-21 05:41:39.595Z | 75.127° E |
| 4 mins | 2026-06-21 07:14:39.595Z | 283.116° WNW | 2026-06-21 07:16:39.595Z | 346.734° N | 27.497° | 2026-06-21 07:18:39.595Z | 30.525° NE |
| 5 mins | 2026-06-21 12:08:39.595Z | 331.274° NNW | 2026-06-21 12:10:39.595Z | 34.274° NE | 32.741° | 2026-06-21 12:13:39.595Z | 101.506° ESE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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