Showing default

KUIPER-00416, 68931

Orbit data source: Space-Track

KUIPER-00416, 68931 is a payload satellite owned by Kuiper Systems (US) in LEO that was launched on Thu, 30 Apr 2026 UTC via an ARIANE 64 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
68931, 2026-098N
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)
2026-04-30 (6 days ago)
Launch vehicle
ARIANE 64
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: 6 hours ago

TLE from 6 hours ago
0 KUIPER-00416
1 68931U 26098N   26126.25002315  .00057024  00000-0  15982-2 0  9992
2 68931  51.8747 269.7120 0002275  78.1530  32.7661 15.36048576  1380
Epoch: 2026-05-06T06:00Z
TLE epoch observation values (Epoch: 2026-05-06T06:00:02.000Z)
Latitude
47.43397°
Longitude
77.4049°
Altitude
461.594 km
Speed
7.643 km/s
True Right ascension
02h 06m 06s
True Declination
47° 15' 19"
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
19:40:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
459.829 km
Perigee altitude
456.719 km
Semi-major axis
6,836.411 km
Eccentricity
0.00023
Inclination
51.8747°
RAAN
269.712°
Arg. of periapsis
78.153°
True anomaly
32.78021°
Mean anomaly
32.7661°
Eccentric anomaly
32.77316°
Mean motion
3.83973 °/min
Orbital period
93.76 mins
BSTAR
0.0015982
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
|