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: 19 hours ago
TLE from 19 hours ago
0 OMNI-L1
1 52157U 22033A 25305.47289597 .00003305 00000-0 42865-3 0 9995
2 52157 97.8603 24.0399 0004246 316.4605 43.6272 14.81449689193723Epoch: 2025-11-01T11:20Z
TLE epoch observation values (Epoch: 2025-11-01T11:20:58.211Z)
Latitude
-0.00006°
Longitude
172.79489°
Altitude
625.624 km
Speed
7.547 km/s
True Right ascension
01h 36m 09s
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
02:28:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
624.761 km
Perigee altitude
618.817 km
Semi-major axis
6,999.926 km
Eccentricity
0.00042
Inclination
97.8603°
RAAN
24.0399°
Arg. of periapsis
316.4605°
True anomaly
43.66078°
Mean anomaly
43.6272°
Eccentric anomaly
43.64399°
Mean motion
3.70598 °/min
Orbital period
97.14 mins
BSTAR
0.00042865
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-11-02 17:08:12.710Z | 66.99° ENE | 2025-11-02 17:10:12.710Z | 98.033° ESE | 14.797° | 2025-11-02 17:12:12.710Z | 126.471° SE |
| 7 mins | 2025-11-02 18:43:12.710Z | 353.284° N | 2025-11-02 18:46:12.710Z | 289.586° WNW | 34.771° | 2025-11-02 18:50:12.710Z | 216.671° SW |
| 6 mins | 2025-11-03 05:38:12.710Z | 186.497° SSW | 2025-11-03 05:40:12.710Z | 239.337° WSW | 40.952° | 2025-11-03 05:44:12.710Z | 338.942° N |
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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