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: 10 hours ago
TLE from 10 hours ago
0 OMNI-L1
1 52157U 22033A 26099.47448058 .00001971 00000-0 25195-3 0 9999
2 52157 97.8399 179.9970 0006294 139.0804 221.0883 14.82498818217271Epoch: 2026-04-09T11:23Z
TLE epoch observation values (Epoch: 2026-04-09T11:23:15.122Z)
Latitude
0.00001°
Longitude
171.46202°
Altitude
627.797 km
Speed
7.543 km/s
True Right ascension
11h 59m 59s
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
03:52:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
622.886 km
Perigee altitude
614.079 km
Semi-major axis
6,996.619 km
Eccentricity
0.00063
Inclination
97.8399°
RAAN
179.997°
Arg. of periapsis
139.0804°
True anomaly
221.04093°
Mean anomaly
221.0883°
Eccentric anomaly
221.06461°
Mean motion
3.70861 °/min
Orbital period
97.07 mins
BSTAR
0.00025195
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-04-10 05:19:10.741Z | 166.359° S | 2026-04-10 05:23:10.741Z | 170.641° S | 44.969° | 2026-04-10 05:27:10.741Z | 347.519° N |
| 4 mins | 2026-04-10 17:09:10.741Z | 65.965° ENE | 2026-04-10 17:11:10.741Z | 98.763° ESE | 15.971° | 2026-04-10 17:13:10.741Z | 128.617° SE |
| 6 mins | 2026-04-10 18:44:10.741Z | 350.209° N | 2026-04-10 18:47:10.741Z | 286.199° WNW | 32.321° | 2026-04-10 18:50:10.741Z | 225.19° WSW |
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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