Showing default

KUIPER-00107, 65145

Orbit data source: Space-Track

KUIPER-00107, 65145 is a payload satellite owned by Kuiper Systems (US) in LEO that was launched on Mon, 11 Aug 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
65145, 2025-171P
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)
2025-08-11 (10 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: 11 hours ago

TLE from 11 hours ago
0 KUIPER-00107
1 65145U 25171P   26171.40103571  .00003020  00000-0  42507-3 0  9991
2 65145  51.9010  53.9056 0000713  98.4433 261.6610 14.79919726 48244
Epoch: 2026-06-20T09:37Z
TLE epoch observation values (Epoch: 2026-06-20T09:37:29.485Z)
Latitude
-0.00003°
Longitude
0.91653°
Altitude
630.397 km
Speed
7.544 km/s
True Right ascension
03h 35m 37s
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
07:12:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.528 km
Perigee altitude
629.529 km
Semi-major axis
7,008.166 km
Eccentricity
0.00007
Inclination
51.901°
RAAN
53.9056°
Arg. of periapsis
98.4433°
True anomaly
261.65292°
Mean anomaly
261.661°
Eccentric anomaly
261.65696°
Mean motion
3.69945 °/min
Orbital period
97.31 mins
BSTAR
0.00042507
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
|