ETV-A1, 51060
Orbit data source: Space-Track
ETV-A1, 51060 is a payload satellite owned by Sen (UK) in SSO that was launched on Thu, 13 Jan 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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51060 intel report (Beta)
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Identifier
Orbit
Country
UKRelated business
Manufacturer
NanoAvionics
Mission
Operational Commercial Imaging
Bus & Motor
CUBESAT 16U, Unknown motor
Mass
~20 kg wet, ~20 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.2 m
Radar Cross Section
0.100 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 ETV-A1
1 51060U 22002CE 26235.92133940 .00010790 00000-0 25529-3 0 9990
2 51060 97.2827 302.0711 0006732 99.0914 261.1096 15.41953840256270Epoch: 2026-08-23T22:06Z
TLE epoch observation values (Epoch: 2026-08-23T22:06:43.724Z)
Latitude
0.00006°
Longitude
-1.82155°
Altitude
444.179 km
Speed
7.645 km/s
True Right ascension
20h 08m 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
02:31:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
441.863 km
Perigee altitude
432.687 km
Semi-major axis
6,815.412 km
Eccentricity
0.00067
Inclination
97.2827°
RAAN
302.0711°
Arg. of periapsis
99.0914°
True anomaly
261.03339°
Mean anomaly
261.1096°
Eccentric anomaly
261.0715°
Mean motion
3.85749 °/min
Orbital period
93.32 mins
BSTAR
0.00025529
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Other satellites on launch #2 in the year 2022 (2022-01-13 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.ETV-A1 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-08-24 17:21:18.284Z | 11.877° NNE | 2026-08-24 17:24:18.284Z | 76.247° E | 44.999° | 2026-08-24 17:27:18.284Z | 192.586° SSW |
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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