OMNI-L2, 52771
Orbit data source: Space-Track
OMNI-L2, 52771 is a payload satellite owned by OmniSpace (US) in SSO that was launched on Wed, 25 May 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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52771 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: 22 hours ago
TLE from 22 hours ago
0 OMNI-L2
1 52771U 22057AR 25348.68296861 .00002267 00000-0 30100-3 0 9990
2 52771 97.4966 58.2926 0006369 198.8365 161.2614 14.80681016193088Epoch: 2025-12-14T16:23Z
TLE epoch observation values (Epoch: 2025-12-14T16:23:28.487Z)
Latitude
-0.00002°
Longitude
88.83154°
Altitude
634.436 km
Speed
7.539 km/s
True Right ascension
03h 53m 10s
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
13:18:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
628.657 km
Perigee altitude
619.738 km
Semi-major axis
7,002.335 km
Eccentricity
0.00064
Inclination
97.4966°
RAAN
58.2926°
Arg. of periapsis
198.8365°
True anomaly
161.28483°
Mean anomaly
161.2614°
Eccentric anomaly
161.27312°
Mean motion
3.70407 °/min
Orbital period
97.19 mins
BSTAR
0.000301
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Other satellites on launch #57 in the year 2022 (2022-05-25 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-L2 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 | 2025-12-15 17:17:13.318Z | 24.821° NE | 2025-12-15 17:21:13.318Z | 103.501° ESE | 36.737° | 2025-12-15 17:25:13.318Z | 173.906° S |
| 6 mins | 2025-12-16 04:13:13.318Z | 124.405° SE | 2025-12-16 04:16:13.318Z | 57.573° ENE | 28.449° | 2025-12-16 04:19:13.318Z | 10.004° NNE |
| 5 mins | 2025-12-16 05:50:13.318Z | 233.813° WSW | 2025-12-16 05:52:13.318Z | 268.649° W | 19.061° | 2025-12-16 05:55:13.318Z | 313.502° NW |
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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