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: 8 hours ago
TLE from 8 hours ago
0 ETV-A1
1 51060U 22002CE 26072.93053748 .00014455 00000-0 38137-3 0 9998
2 51060 97.2986 139.6097 0004455 345.7479 14.3641 15.38570880231186Epoch: 2026-03-13T22:19Z
TLE epoch observation values (Epoch: 2026-03-13T22:19:58.438Z)
Latitude
0.00008°
Longitude
-6.94281°
Altitude
450.505 km
Speed
7.644 km/s
True Right ascension
09h 18m 26s
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
10:49:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
450.312 km
Perigee altitude
444.23 km
Semi-major axis
6,825.408 km
Eccentricity
0.00045
Inclination
97.2986°
RAAN
139.6097°
Arg. of periapsis
345.7479°
True anomaly
14.37677°
Mean anomaly
14.3641°
Eccentric anomaly
14.37044°
Mean motion
3.84902 °/min
Orbital period
93.53 mins
BSTAR
0.00038137
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-03-14 17:37:37.218Z | 349.617° N | 2026-03-14 17:39:37.218Z | 297.692° NW | 32.744° | 2026-03-14 17:42:37.218Z | 217.64° SW |
| 4 mins | 2026-03-15 04:08:37.218Z | 133.03° SE | 2026-03-15 04:09:37.218Z | 100.596° ESE | 34.726° | 2026-03-15 04:12:37.218Z | 3.868° NNE |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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