Showing default

KUIPER-00191, 67143

Orbit data source: Space-Track

KUIPER-00191, 67143 is a payload satellite owned by Kuiper Systems (US) in LEO that was launched on Mon, 15 Dec 2025 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
67143, 2025-301L
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
Kuiper Systems
Mission
Operational Commercial Communications
Bus & Motor
KUIPER, Unknown motor
Mass
~490 kg wet, ~490 kg dry
Launch date (UTC)
2025-12-15 (6 months ago)
Launch vehicle
ATLAS V 551
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 3.4 m
Radar Cross Section
2.326 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 9 hours ago

TLE from 9 hours ago
0 KUIPER-00191
1 67143U 25301L   26171.46509753  .00002815  00000-0  39810-3 0  9998
2 67143  51.9016 338.6747 0000622 100.3181 259.7851 14.79933239 28879
Epoch: 2026-06-20T11:09Z
TLE epoch observation values (Epoch: 2026-06-20T11:09:44.426Z)
Latitude
-0.00006°
Longitude
-97.43979°
Altitude
630.359 km
Speed
7.544 km/s
True Right ascension
22h 34m 41s
True Declination
0° 00' 00"
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
07:16:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.422 km
Perigee altitude
629.55 km
Semi-major axis
7,008.123 km
Eccentricity
0.00006
Inclination
51.9016°
RAAN
338.6747°
Arg. of periapsis
100.3181°
True anomaly
259.77809°
Mean anomaly
259.7851°
Eccentric anomaly
259.78159°
Mean motion
3.69948 °/min
Orbital period
97.31 mins
BSTAR
0.0003981
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
|