Showing default

KUIPER-00165, 65778

Orbit data source: Space-Track

KUIPER-00165, 65778 is a payload satellite owned by Kuiper Systems (US) in LEO that was launched on Thu, 25 Sep 2025 UTC via an ATLAS V 551 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
65778, 2025-217S
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)
2025-09-25 (9 months ago)
Launch vehicle
ATLAS V 551
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-00165
1 65778U 25217S   26170.62765990  .00002864  00000-0  40452-3 0  9998
2 65778  51.9010 304.8329 0000520 107.7419 252.3600 14.79932292 40073
Epoch: 2026-06-19T15:03Z
TLE epoch observation values (Epoch: 2026-06-19T15:03:49.815Z)
Latitude
-0.00002°
Longitude
171.0214°
Altitude
630.395 km
Speed
7.544 km/s
True Right ascension
20h 19m 19s
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
08:32:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.353 km
Perigee altitude
629.624 km
Semi-major axis
7,008.126 km
Eccentricity
0.00005
Inclination
51.901°
RAAN
304.8329°
Arg. of periapsis
107.7419°
True anomaly
252.35432°
Mean anomaly
252.36°
Eccentric anomaly
252.35716°
Mean motion
3.69948 °/min
Orbital period
97.31 mins
BSTAR
0.00040452
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
|