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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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: 12 hours ago
TLE from 12 hours ago
0 OMNI-L1
1 52157U 22033A 26042.16514490 .00002607 00000-0 33359-3 0 9995
2 52157 97.8483 123.8038 0004676 350.0224 10.0896 14.82191381208782Epoch: 2026-02-11T03:57Z
TLE epoch observation values (Epoch: 2026-02-11T03:57:48.519Z)
Latitude
0.00002°
Longitude
-76.88354°
Altitude
622.218 km
Speed
7.549 km/s
True Right ascension
08h 15m 12s
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
18:35:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
622.723 km
Perigee altitude
616.179 km
Semi-major axis
6,997.588 km
Eccentricity
0.00047
Inclination
97.8483°
RAAN
123.8038°
Arg. of periapsis
350.0224°
True anomaly
10.09899°
Mean anomaly
10.0896°
Eccentric anomaly
10.0943°
Mean motion
3.70784 °/min
Orbital period
97.09 mins
BSTAR
0.00033359
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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 | 2026-02-11 17:30:38.725Z | 42.857° NE | 2026-02-11 17:33:38.725Z | 98.458° ESE | 25.594° | 2026-02-11 17:36:38.725Z | 151.288° SSE |
| 5 mins | 2026-02-11 19:07:38.725Z | 328.455° NNW | 2026-02-11 19:09:38.725Z | 290.224° WNW | 22.07° | 2026-02-11 19:12:38.725Z | 241.778° WSW |
| 5 mins | 2026-02-12 04:25:38.725Z | 104.753° ESE | 2026-02-12 04:27:38.725Z | 69.757° E | 20.215° | 2026-02-12 04:30:38.725Z | 21.418° NNE |
| 5 mins | 2026-02-12 06:01:38.725Z | 216.738° SW | 2026-02-12 06:03:38.725Z | 261.112° W | 27.607° | 2026-02-12 06:06:38.725Z | 319.432° 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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