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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52157 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
NANAV/THALES
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 12U, Unknown motor
Mass
~20 kg wet, ~20 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
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 & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 OMNI-L1
1 52157U 22033A 25358.95863323 .00002914 00000-0 37491-3 0 9995
2 52157 97.8554 76.5135 0006382 126.4417 233.7385 14.81860983201643Epoch: 2025-12-24T23:00Z
TLE epoch observation values (Epoch: 2025-12-24T23:00:25.911Z)
Latitude
-0.00002°
Longitude
-2.31501°
Altitude
629.127 km
Speed
7.542 km/s
True Right ascension
05h 06m 03s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
12:42:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
624.959 km
Perigee altitude
616.026 km
Semi-major axis
6,998.629 km
Eccentricity
0.00064
Inclination
97.8554°
RAAN
76.5135°
Arg. of periapsis
126.4417°
True anomaly
233.67956°
Mean anomaly
233.7385°
Eccentric anomaly
233.70903°
Mean motion
3.70701 °/min
Orbital period
97.11 mins
BSTAR
0.00037491
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Other satellites on launch #33 in the year 2022 (2022-04-01 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.OMNI-L1 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-25 17:25:12.186Z | 46.002° ENE | 2025-12-25 17:28:12.186Z | 97.953° ESE | 22.345° | 2025-12-25 17:31:12.186Z | 146.869° SSE |
| 5 mins | 2025-12-25 19:02:12.186Z | 331.959° NNW | 2025-12-25 19:04:12.186Z | 290.817° WNW | 24.713° | 2025-12-25 19:07:12.186Z | 237.917° WSW |
| 4 mins | 2025-12-26 04:21:12.186Z | 90.09° ESE | 2025-12-26 04:22:12.186Z | 72.813° E | 17.811° | 2025-12-26 04:25:12.186Z | 25.559° NE |
| 6 mins | 2025-12-26 05:56:12.186Z | 208.693° SW | 2025-12-26 05:58:12.186Z | 254.056° W | 30.846° | 2025-12-26 06:02:12.186Z | 328.888° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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