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: 6 hours ago
TLE from 6 hours ago
0 OMNI-L1
1 52157U 22033A 25299.12378573 .00002979 00000-0 38733-3 0 9997
2 52157 97.8602 17.8122 0004657 340.6518 19.4518 14.81405873192780Epoch: 2025-10-26T02:58Z
TLE epoch observation values (Epoch: 2025-10-26T02:58:15.087Z)
Latitude
0.00007°
Longitude
-61.49517°
Altitude
624.839 km
Speed
7.548 km/s
True Right ascension
01h 11m 14s
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
04:16:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
625.187 km
Perigee altitude
618.667 km
Semi-major axis
7,000.064 km
Eccentricity
0.00047
Inclination
97.8602°
RAAN
17.8122°
Arg. of periapsis
340.6518°
True anomaly
19.46958°
Mean anomaly
19.4518°
Eccentric anomaly
19.46069°
Mean motion
3.70587 °/min
Orbital period
97.14 mins
BSTAR
0.00038733
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-10-26 18:07:54.310Z | 17.639° NNE | 2025-10-26 18:11:54.310Z | 153.506° SSE | 42.204° | 2025-10-26 18:14:54.310Z | 186.104° SSW |
| 7 mins | 2025-10-27 05:01:54.310Z | 147.748° SSE | 2025-10-27 05:05:54.310Z | 57.986° ENE | 37.859° | 2025-10-27 05:08:54.310Z | 1.296° NNE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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