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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Edit Public Description
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: 18 hours ago
TLE from 18 hours ago
0 ETV-A1
1 51060U 22002CE 25287.29060950 .00012940 00000-0 39240-3 0 9990
2 51060 97.3239 349.8894 0007008 139.8088 220.3674 15.34228052208055Epoch: 2025-10-14T06:58Z
TLE epoch observation values (Epoch: 2025-10-14T06:58:28.660Z)
Latitude
-0.00009°
Longitude
-137.81116°
Altitude
469.981 km
Speed
7.629 km/s
True Right ascension
23h 19m 33s
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
19:40:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
464.95 km
Perigee altitude
455.365 km
Semi-major axis
6,838.295 km
Eccentricity
0.0007
Inclination
97.3239°
RAAN
349.8894°
Arg. of periapsis
139.8088°
True anomaly
220.31542°
Mean anomaly
220.3674°
Eccentric anomaly
220.34141°
Mean motion
3.83815 °/min
Orbital period
93.8 mins
BSTAR
0.0003924
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-10-15 03:28:39.589Z | 107.661° ESE | 2025-10-15 03:30:39.589Z | 69.076° E | 16.719° | 2025-10-15 03:32:39.589Z | 30.513° NE |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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