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 (2 months ago)
Launch vehicle
ATLAS V 551
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 3.4 m
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 KUIPER-00285
1 68589U 26072S   26149.54296333  .00035029  00000-0  91325-3 0  9992
2 68589  51.8741 266.9733 0007022 307.7986  52.2365 15.38492622  8510
Epoch: 2026-05-29T13:01Z
TLE epoch observation values (Epoch: 2026-05-29T13:01:52.031Z)
Latitude
-0.00002°
Longitude
-175.56535°
Altitude
448.395 km
Speed
7.646 km/s
True Right ascension
17h 47m 53s
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
01:23:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
455.829 km
Perigee altitude
446.238 km
Semi-major axis
6,829.17 km
Eccentricity
0.0007
Inclination
51.8741°
RAAN
266.9733°
Arg. of periapsis
307.7986°
True anomaly
52.30015°
Mean anomaly
52.2365°
Eccentric anomaly
52.26832°
Mean motion
3.84584 °/min
Orbital period
93.61 mins
BSTAR
0.00091325
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
|