Showing default

KUIPER-00453, 68947

Orbit data source: Space-Track

KUIPER-00453, 68947 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
68947, 2026-098AE
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: 7 hours ago

TLE from 7 hours ago
0 KUIPER-00453
1 68947U 26098AE  26126.25002315  .00055944  00000-0  15777-2 0  9990
2 68947  51.8747 269.7225 0002832  60.3587  45.3618 15.35862692  1628
Epoch: 2026-05-06T06:00Z
TLE epoch observation values (Epoch: 2026-05-06T06:00:02.000Z)
Latitude
49.36518°
Longitude
70.16936°
Altitude
462.533 km
Speed
7.642 km/s
True Right ascension
01h 37m 09s
True Declination
49° 11' 16"
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
21:14:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
460.762 km
Perigee altitude
456.889 km
Semi-major axis
6,836.963 km
Eccentricity
0.00028
Inclination
51.8747°
RAAN
269.7225°
Arg. of periapsis
60.3587°
True anomaly
45.3849°
Mean anomaly
45.3618°
Eccentric anomaly
45.37335°
Mean motion
3.83927 °/min
Orbital period
93.77 mins
BSTAR
0.0015777
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
|