Showing default

KUIPER-00608, 69291

Orbit data source: Space-Track

KUIPER-00608, 69291 is a payload satellite owned by Kuiper Systems (US) in LEO that was launched on Fri, 29 May 2026 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
69291, 2026-118AA
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
Kuiper Systems
Mission
Operational spacecraft
Bus & Motor
KUIPER, Unknown motor
Mass
~490 kg wet, ~490 kg dry
Launch date (UTC)
2026-05-29 (3 weeks ago)
Launch vehicle
ATLAS V 551
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 14 hours ago

TLE from 14 hours ago
0 KUIPER-00608
1 69291U 26118AA  26171.33600023  .00016365  00000-0  48004-3 0  9999
2 69291  51.8610  38.2683 0008361 187.5435 172.5426 15.35280130  4460
Epoch: 2026-06-20T08:03Z
TLE epoch observation values (Epoch: 2026-06-20T08:03:50.419Z)
Latitude
-0.00006°
Longitude
8.75609°
Altitude
466.518 km
Speed
7.631 km/s
True Right ascension
02h 33m 04s
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
08:32:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
466.275 km
Perigee altitude
454.839 km
Semi-major axis
6,838.694 km
Eccentricity
0.00084
Inclination
51.861°
RAAN
38.2683°
Arg. of periapsis
187.5435°
True anomaly
172.55502°
Mean anomaly
172.5426°
Eccentric anomaly
172.54881°
Mean motion
3.83781 °/min
Orbital period
93.8 mins
BSTAR
0.00048004
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
|