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OMNI-L1, 52157

Orbit data source: Space-Track

OMNI-L1, 52157 is a payload satellite owned by OmniSpace (US) in SSO that was launched on Fri, 01 Apr 2022 UTC via an FALCON 9 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.

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Identifier
52157, 2022-033A
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
NANAV/THALES
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 12U, Unknown motor
Mass
~20 kg wet, ~20 kg dry
Launch date (UTC)
2022-04-01 (4 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 0.5 m
Radar Cross Section
0.126 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 8 hours ago

TLE from 8 hours ago
0 OMNI-L1
1 52157U 22033A   25352.20615012  .00002088  00000-0  27074-3 0  9995
2 52157  97.8570  69.8888 0006083 144.7149 215.4468 14.81827662200649
Epoch: 2025-12-18T04:56Z
TLE epoch observation values (Epoch: 2025-12-18T04:56:51.370Z)
Latitude
0.00001°
Longitude
-91.39023°
Altitude
630.058 km
Speed
7.542 km/s
True Right ascension
04h 39m 33s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
11:56:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
624.855 km
Perigee altitude
616.34 km
Semi-major axis
6,998.735 km
Eccentricity
0.00061
Inclination
97.857°
RAAN
69.8888°
Arg. of periapsis
144.7149°
True anomaly
215.4064°
Mean anomaly
215.4468°
Eccentric anomaly
215.4266°
Mean motion
3.70693 °/min
Orbital period
97.12 mins
BSTAR
0.00027074
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