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KUIPER-00134, 65960

Orbit data source: Space-Track

KUIPER-00134, 65960 is a payload satellite owned by Kuiper Systems (US) in LEO that was launched on Tue, 14 Oct 2025 UTC via an FALCON 9 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
65960, 2025-228P
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
Kuiper Systems
Mission
Operational Commercial Communications
Bus & Motor
KUIPER, Unknown motor
Mass
~490 kg wet, ~490 kg dry
Launch date (UTC)
2025-10-14 (8 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 3.4 m
Radar Cross Section
2.326 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 KUIPER-00134
1 65960U 25228P   26170.33685198  .00027753  00000-0  66326-3 0  9994
2 65960  51.8699 186.8739 0006795 323.8875  36.1654 15.41266881 39459
Epoch: 2026-06-19T08:05Z
TLE epoch observation values (Epoch: 2026-06-19T08:05:04.011Z)
Latitude
0.00002°
Longitude
158.03992°
Altitude
439.393 km
Speed
7.652 km/s
True Right ascension
12h 27m 29s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
07:16:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
447.472 km
Perigee altitude
438.203 km
Semi-major axis
6,820.974 km
Eccentricity
0.00068
Inclination
51.8699°
RAAN
186.8739°
Arg. of periapsis
323.8875°
True anomaly
36.21138°
Mean anomaly
36.1654°
Eccentric anomaly
36.18839°
Mean motion
3.85277 °/min
Orbital period
93.44 mins
BSTAR
0.00066326
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Documentation

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