Showing default

KUIPER-00285, 68589

Orbit data source: Space-Track

KUIPER-00285, 68589 is a payload satellite owned by Kuiper Systems (US) in LEO that was launched on Sat, 04 Apr 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
68589, 2026-072S
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)
2026-04-04 (1 week 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
RCS unknown

Expand to show TLE details & history
Last TLE update: 10 hours ago

TLE from 10 hours ago
0 KUIPER-00285
1 68589U 26072S   26101.50002315  .00052771  00000-0  14256-2 0  9991
2 68589  51.8731 139.4414 0006428 128.8791 126.3494 15.37210724  2198
Epoch: 2026-04-11T12:00Z
TLE epoch observation values (Epoch: 2026-04-11T12:00:02.000Z)
Latitude
-49.70652°
Longitude
6.72404°
Altitude
473.958 km
Speed
7.627 km/s
True Right ascension
01h 45m 48s
True Declination
-49° 31' 47"
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
04:00:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
459.221 km
Perigee altitude
450.437 km
Semi-major axis
6,832.966 km
Eccentricity
0.00064
Inclination
51.8731°
RAAN
139.4414°
Arg. of periapsis
128.8791°
True anomaly
126.4087°
Mean anomaly
126.3494°
Eccentric anomaly
126.37905°
Mean motion
3.84264 °/min
Orbital period
93.69 mins
BSTAR
0.0014256
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
|