Showing default

KUIPER-00113, 65948

Orbit data source: Space-Track

KUIPER-00113, 65948 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.

Loading next visibility...
Identifier
65948, 2025-228B
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: 10 hours ago

TLE from 10 hours ago
0 KUIPER-00113
1 65948U 25228B   26171.44739010  .00001026  00000-0  16356-3 0  9999
2 65948  51.8968 261.1849 0000553  97.1656 262.9369 14.79929601 38511
Epoch: 2026-06-20T10:44Z
TLE epoch observation values (Epoch: 2026-06-20T10:44:14.504Z)
Latitude
-0.00004°
Longitude
-168.53745°
Altitude
630.34 km
Speed
7.544 km/s
True Right ascension
17h 24m 44s
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
07:14:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.386 km
Perigee altitude
629.61 km
Semi-major axis
7,008.135 km
Eccentricity
0.00006
Inclination
51.8968°
RAAN
261.1849°
Arg. of periapsis
97.1656°
True anomaly
262.93061°
Mean anomaly
262.9369°
Eccentric anomaly
262.93376°
Mean motion
3.69947 °/min
Orbital period
97.31 mins
BSTAR
0.00016356
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|