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: 1 day ago
TLE from 1 day ago
0 OMNI-L1
1 52157U 22033A 25255.68748831 .00001619 00000-0 21526-3 0 9990
2 52157 97.8640 335.2075 0006767 107.2644 252.9309 14.81069608186357Epoch: 2025-09-12T16:29Z
TLE epoch observation values (Epoch: 2025-09-12T16:29:58.989Z)
Latitude
-0.00011°
Longitude
95.78011°
Altitude
630.368 km
Speed
7.542 km/s
True Right ascension
22h 20m 49s
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
20:43:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
627.725 km
Perigee altitude
618.25 km
Semi-major axis
7,001.125 km
Eccentricity
0.00068
Inclination
97.864°
RAAN
335.2075°
Arg. of periapsis
107.2644°
True anomaly
252.85679°
Mean anomaly
252.9309°
Eccentric anomaly
252.89384°
Mean motion
3.70503 °/min
Orbital period
97.17 mins
BSTAR
0.00021526
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-09-14 04:19:39.204Z | 105.202° ESE | 2025-09-14 04:22:39.204Z | 58.39° ENE | 16.955° | 2025-09-14 04:24:39.204Z | 28.636° NE |
| 6 mins | 2025-09-14 05:55:39.204Z | 203.588° SW | 2025-09-14 05:57:39.204Z | 244.507° WSW | 31.479° | 2025-09-14 06:01:39.204Z | 328.428° NNW |
| 6 mins | 2025-09-14 17:43:39.204Z | 37.578° NE | 2025-09-14 17:46:39.204Z | 101.29° ESE | 30.87° | 2025-09-14 17:49:39.204Z | 159.887° S |
| 4 mins | 2025-09-14 19:20:39.204Z | 324.629° NNW | 2025-09-14 19:22:39.204Z | 290.693° WNW | 17.963° | 2025-09-14 19:24:39.204Z | 258.358° W |
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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