Showing default

KUIPER-00091, 64836

Orbit data source: Space-Track

KUIPER-00091, 64836 is a payload satellite owned by Kuiper Systems (US) in LEO that was launched on Wed, 16 Jul 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
64836, 2025-151W
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)
2025-07-16 (11 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: 19 hours ago

TLE from 19 hours ago
0 KUIPER-00091
1 64836U 25151W   26166.39332535 -.00000474  00000-0 -33233-4 0  9990
2 64836  51.8998 211.0651 0000462  80.7488 279.3526 14.79927535 50014
Epoch: 2026-06-15T09:26Z
TLE epoch observation values (Epoch: 2026-06-15T09:26:23.310Z)
Latitude
-0.00005°
Longitude
165.78758°
Altitude
630.247 km
Speed
7.545 km/s
True Right ascension
14h 04m 15s
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
14:43:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.328 km
Perigee altitude
629.68 km
Semi-major axis
7,008.141 km
Eccentricity
0.00005
Inclination
51.8998°
RAAN
211.0651°
Arg. of periapsis
80.7488°
True anomaly
279.34738°
Mean anomaly
279.3526°
Eccentric anomaly
279.34999°
Mean motion
3.69946 °/min
Orbital period
97.31 mins
BSTAR
-0.000033233
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
|