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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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: 2 days ago
TLE from 2 days ago
0 OMNI-L2
1 52771U 22057AR 26171.43231169 .00000980 00000-0 13144-3 0 9997
2 52771 97.4714 233.5727 0005521 324.4275 35.6570 14.81377450220870Epoch: 2026-06-20T10:22Z
TLE epoch observation values (Epoch: 2026-06-20T10:22:31.730Z)
Latitude
-0.00002°
Longitude
169.29347°
Altitude
624.874 km
Speed
7.548 km/s
True Right ascension
15h 34m 17s
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
21:44:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
625.865 km
Perigee altitude
618.135 km
Semi-major axis
7,000.137 km
Eccentricity
0.00055
Inclination
97.4714°
RAAN
233.5727°
Arg. of periapsis
324.4275°
True anomaly
35.6939°
Mean anomaly
35.657°
Eccentric anomaly
35.67545°
Mean motion
3.70581 °/min
Orbital period
97.14 mins
BSTAR
0.00013144
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-22 16:26:33.143Z | 31.032° NE | 2026-06-22 16:30:33.143Z | 103.713° ESE | 30.364° | 2026-06-22 16:33:33.143Z | 159.201° S |
| 4 mins | 2026-06-22 18:04:33.143Z | 323.299° NNW | 2026-06-22 18:06:33.143Z | 288.758° WNW | 18.427° | 2026-06-22 18:08:33.143Z | 256.587° W |
| 5 mins | 2026-06-23 03:22:33.143Z | 111.514° ESE | 2026-06-23 03:24:33.143Z | 74.703° E | 23.108° | 2026-06-23 03:27:33.143Z | 20.941° NNE |
| 6 mins | 2026-06-23 04:58:33.143Z | 218.978° SW | 2026-06-23 05:00:33.143Z | 255.42° W | 23.863° | 2026-06-23 05:04:33.143Z | 322.409° NNW |
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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