Showing default

KUIPER-00605, 69288

Orbit data source: Space-Track

KUIPER-00605, 69288 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
69288, 2026-118X
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: 20 hours ago

TLE from 20 hours ago
0 KUIPER-00605
1 69288U 26118X   26170.99525921  .00013636  00000-0  37935-3 0  9998
2 69288  51.8662  39.7473 0007383 177.8626 182.2393 15.37104765  4410
Epoch: 2026-06-19T23:53Z
TLE epoch observation values (Epoch: 2026-06-19T23:53:10.395Z)
Latitude
-0.00006°
Longitude
133.2377°
Altitude
460.479 km
Speed
7.635 km/s
True Right ascension
02h 38m 59s
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
07:12:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
460.189 km
Perigee altitude
450.099 km
Semi-major axis
6,833.281 km
Eccentricity
0.00074
Inclination
51.8662°
RAAN
39.7473°
Arg. of periapsis
177.8626°
True anomaly
182.236°
Mean anomaly
182.2393°
Eccentric anomaly
182.23765°
Mean motion
3.84237 °/min
Orbital period
93.69 mins
BSTAR
0.00037935
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
|