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: 17 hours ago
TLE from 17 hours ago
0 OMNI-L2
1 52771U 22057AR 26091.18137548 .00001741 00000-0 23004-3 0 9998
2 52771 97.4775 158.7034 0006145 204.8537 155.2382 14.81153827208990Epoch: 2026-04-01T04:21Z
TLE epoch observation values (Epoch: 2026-04-01T04:21:10.841Z)
Latitude
0.00001°
Longitude
-96.13967°
Altitude
632.629 km
Speed
7.54 km/s
True Right ascension
10h 34m 48s
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
03:11:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
627.007 km
Perigee altitude
618.403 km
Semi-major axis
7,000.842 km
Eccentricity
0.00061
Inclination
97.4775°
RAAN
158.7034°
Arg. of periapsis
204.8537°
True anomaly
155.26767°
Mean anomaly
155.2382°
Eccentric anomaly
155.25294°
Mean motion
3.70525 °/min
Orbital period
97.16 mins
BSTAR
0.00023004
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-04-02 03:13:20.945Z | 92.158° ESE | 2026-04-02 03:15:20.945Z | 63.705° ENE | 13.463° | 2026-04-02 03:17:20.945Z | 35.67° NE |
| 6 mins | 2026-04-02 04:48:20.945Z | 189.627° SSW | 2026-04-02 04:51:20.945Z | 275.411° WNW | 38.571° | 2026-04-02 04:54:20.945Z | 334.354° NNW |
| 5 mins | 2026-04-02 16:37:20.945Z | 51.252° ENE | 2026-04-02 16:39:20.945Z | 93.007° ESE | 26.075° | 2026-04-02 16:42:20.945Z | 149.819° SSE |
| 5 mins | 2026-04-02 18:13:20.945Z | 331.38° NNW | 2026-04-02 18:15:20.945Z | 296.199° NW | 21.384° | 2026-04-02 18:18:20.945Z | 245.019° 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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