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KUIPER-00130, 65959

Orbit data source: Space-Track

KUIPER-00130, 65959 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
65959, 2025-228N
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: 1 day ago

TLE from 1 day ago
0 KUIPER-00130
1 65959U 25228N   26170.54113365  .00002403  00000-0  34410-3 0  9991
2 65959  51.9022 260.2497 0000450  94.4153 265.6861 14.79938467 28743
Epoch: 2026-06-19T12:59Z
TLE epoch observation values (Epoch: 2026-06-19T12:59:13.947Z)
Latitude
Longitude
157.67296°
Altitude
630.289 km
Speed
7.544 km/s
True Right ascension
17h 20m 59s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
07:16:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.285 km
Perigee altitude
629.654 km
Semi-major axis
7,008.106 km
Eccentricity
0.00005
Inclination
51.9022°
RAAN
260.2497°
Arg. of periapsis
94.4153°
True anomaly
265.68096°
Mean anomaly
265.6861°
Eccentric anomaly
265.68353°
Mean motion
3.69949 °/min
Orbital period
97.31 mins
BSTAR
0.0003441
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