Showing default

KUIPER-00478, 68875

Orbit data source: Space-Track

KUIPER-00478, 68875 is an American payload satellite in LEO that was launched on Tue, 28 Apr 2026 UTC launched 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
68875, 2026-095M
Orbit
LEO
Country
Flag of USUS
Related business
None
Manufacturer
Unknown
Mission
Operational spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
2026-04-28 (4 days ago)
Launch vehicle
Unknown
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-00478
1 68875U 26095M   26122.16670139 -.00002951  00000-0 -70711-4 0  9991
2 68875  51.8763 104.9364 0008501 129.1637  61.9759 15.36482197  1303
Epoch: 2026-05-02T04:00Z
TLE epoch observation values (Epoch: 2026-05-02T04:00:03.000Z)
Latitude
-8.93857°
Longitude
11.88615°
Altitude
456.149 km
Speed
7.641 km/s
True Right ascension
19h 27m 56s
True Declination
-8° 53' 01"
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
18:39:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
462.798 km
Perigee altitude
451.177 km
Semi-major axis
6,835.125 km
Eccentricity
0.00085
Inclination
51.8763°
RAAN
104.9364°
Arg. of periapsis
129.1637°
True anomaly
62.06194°
Mean anomaly
61.9759°
Eccentric anomaly
62.01891°
Mean motion
3.84082 °/min
Orbital period
93.73 mins
BSTAR
-0.000070711
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
|