Showing default

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.

Loading next visibility...
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 (3 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: 17 hours ago

TLE from 17 hours ago
0 OMNI-L1
1 52157U 22033A   25260.01130275  .00001893  00000-0  25050-3 0  9990
2 52157  97.8635 339.4484 0006809  96.0225 264.1763 14.81086873186990
Epoch: 2025-09-17T00:16Z
TLE epoch observation values (Epoch: 2025-09-17T00:16:16.557Z)
Latitude
-0.0001°
Longitude
-20.81395°
Altitude
629.407 km
Speed
7.543 km/s
True Right ascension
22h 37m 47s
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
09:55:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
627.7 km
Perigee altitude
618.166 km
Semi-major axis
7,001.07 km
Eccentricity
0.00068
Inclination
97.8635°
RAAN
339.4484°
Arg. of periapsis
96.0225°
True anomaly
264.09868°
Mean anomaly
264.1763°
Eccentric anomaly
264.13749°
Mean motion
3.70507 °/min
Orbital period
97.16 mins
BSTAR
0.0002505
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|