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: 9 hours ago
TLE from 9 hours ago
0 OMNI-L1
1 52157U 22033A 26264.73798938 .00000987 00000-0 12774-3 0 9992
2 52157 97.8331 342.0243 0004559 344.5524 15.5550 14.83028991241767Epoch: 2026-09-21T17:42Z
TLE epoch observation values (Epoch: 2026-09-21T17:42:42.282Z)
Latitude
-0.00001°
Longitude
75.73461°
Altitude
619.733 km
Speed
7.551 km/s
True Right ascension
22h 48m 05s
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
20:13:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
620.002 km
Perigee altitude
613.624 km
Semi-major axis
6,994.95 km
Eccentricity
0.00046
Inclination
97.8331°
RAAN
342.0243°
Arg. of periapsis
344.5524°
True anomaly
15.56902°
Mean anomaly
15.555°
Eccentric anomaly
15.56201°
Mean motion
3.70993 °/min
Orbital period
97.04 mins
BSTAR
0.00012774
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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 | 2026-09-22 05:10:16.027Z | 160.414° S | 2026-09-22 05:13:16.027Z | 131.425° SE | 68.101° | 2026-09-22 05:17:16.027Z | 351.403° N |
| 7 mins | 2026-09-22 18:34:16.027Z | 355.144° N | 2026-09-22 18:37:16.027Z | 293.576° NW | 46.315° | 2026-09-22 18:41:16.027Z | 215.296° SW |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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