Showing default

KUIPER-00297, 68596

Orbit data source: Space-Track

KUIPER-00297, 68596 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
68596, 2026-072Z
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 (1 week ago)
Launch vehicle
ATLAS V 551
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: 11 hours ago

TLE from 11 hours ago
0 KUIPER-00297
1 68596U 26072Z   26101.50002315  .00051823  00000-0  14508-2 0  9996
2 68596  51.8620 139.5050 0010292 142.4189  83.0556 15.36080801  2139
Epoch: 2026-04-11T12:00Z
TLE epoch observation values (Epoch: 2026-04-11T12:00:02.000Z)
Latitude
-34.39026°
Longitude
-27.91532°
Altitude
467.605 km
Speed
7.633 km/s
True Right ascension
23h 27m 14s
True Declination
-34° 13' 24"
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
05:47:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
465.217 km
Perigee altitude
451.145 km
Semi-major axis
6,836.318 km
Eccentricity
0.00103
Inclination
51.862°
RAAN
139.505°
Arg. of periapsis
142.4189°
True anomaly
83.17269°
Mean anomaly
83.0556°
Eccentric anomaly
83.11414°
Mean motion
3.83981 °/min
Orbital period
93.75 mins
BSTAR
0.0014508
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
|