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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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Iframe URL

https://www.satcat.com/sats-embedded/51060?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

51060, 2022-002CE

Orbit

SSO

Last TLE update

9 hours ago

Origin

Sen Corporation Ltd (UK)

Manufacturer

NanoAvionics

Mission

Operational Commercial Imaging

Bus & Motor

CUBESAT 16U, Unknown motor

Mass

~20 kg wet, ~20 kg dry

Launch date (UTC)

2022-01-13 (4 years ago)

Launch vehicle

FALCON 9

Launch site

Air Force Eastern Test Range (AFETR)

Object type

Payload

Rocket body

Debris

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 & history

TLE from 9 hours ago

0 ETV-A1
1 51060U 22002CE  25202.89795353  .00006490  00000-0  21057-3 0  9995
2 51060  97.3367 266.2270 0007977  92.6839 267.5316 15.32275439195120

Epoch: 2025-07-21T21:33Z

TLE epoch observation values (Epoch: 2025-07-21T21:33:03.184Z)

Latitude

-0.00007°

Longitude

3.06399°

Altitude

472.374 km

Speed

7.63 km/s

True Right ascension

17h 44m 54s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

Latitude

-59.21565°

Longitude

15.85288°

Altitude

496.71 km

Speed

7.612 km/s

Apparent Right ascension

09h 56m 12s

Apparent Declination

-79° 38' 13"

Sunlit

Object is in full shadow

Visualization observer readout

Local Sidereal Time

19:42:14

Azimuth

188.576° SSW

Elevation

-48.268°

Doppler factor

Orbital elements

Apogee altitude

471.431 km

Perigee altitude

460.512 km

Semi-major axis

6,844.109 km

Eccentricity

0.0008

Inclination

97.3367°

RAAN

266.227°

Arg. of periapsis

92.6839°

True anomaly

267.44028°

Mean anomaly

267.5316°

Eccentric anomaly

267.48594°

Mean motion

3.83326 °/min

Orbital period

93.91 mins

BSTAR

0.00021057

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Other satellites on launch #2 in the year 2022 (2022-01-13 UTC)

FOSSASAT2E2, 50984 (Decayed)

ICEYE-X16, 51008 (Decayed)

FLOCK 4X 37, 51009 (Decayed)

FLOCK 4X 15, 51010 (Decayed)

FLOCK 4X 29, 51011 (Decayed)

FLOCK 4X 27, 51012 (Decayed)

TEVEL 1, 51013 (Decayed)

SATLLA-2B, 51014 (Decayed)

FLOCK 4X 12, 51015 (Decayed)

FLOCK 4X 25, 51016 (Decayed)

FLOCK 4X 1, 51017 (Decayed)

FLOCK 4X 42, 51018 (Decayed)

OBJECT AM, 51019 (Decayed)

FLOCK 4X 16, 51020 (Decayed)

LEMUR 2 RAMONAMAE, 51021 (Decayed)

ETV-A1 Visibility forecast

Observer location: undefined°, undefined°

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	2025-07-22 16:55:37.292Z	23.985° NE	2025-07-22 16:57:37.292Z	65.194° ENE	38.633°	2025-07-22 17:00:37.292Z	177.572° S
4 mins	2025-07-23 05:02:37.292Z	231.559° WSW	2025-07-23 05:03:37.292Z	254.928° W	20.407°	2025-07-23 05:06:37.292Z	316.476° 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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Authenticating...

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Check out ETV-A1, 51060 on other resources

View ETV-A1, 51060 on NASA - NSSDCA Website

View ETV-A1, 51060 on Heavens-Above

View ETV-A1, 51060 on Keep Track

View ETV-A1, 51060 on Celestrak

View ETV-A1, 51060 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.