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VIGORIDE 3, 52760

Orbit data source: Space-Track

VIGORIDE 3, 52760 is a payload satellite owned by Momentus (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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Iframe URL

https://www.satcat.com/sats-embedded/52760?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

52760, 2022-057AE

Orbit

SSO

Last TLE update

1 day ago

Origin

Momentus Space (US)

Manufacturer

Momentus

Mission

Operational Commercial Technology

Bus & Motor

VIGORIDE, AOCS

Mass

412 kg wet, 292 kg dry

Launch date (UTC)

2022-05-25 (3 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, 3.3 m

Radar Cross Section

1.548 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 1 day ago

0 VIGORIDE 3
1 52760U 22057AE  25232.88431736  .00003369  00000-0  14508-3 0  9992
2 52760  97.6212   1.6400 0011059  95.1486 265.1012 15.23271049179388

Epoch: 2025-08-20T21:13Z

TLE epoch observation values (Epoch: 2025-08-20T21:13:25.019Z)

Latitude

-0.00012°

Longitude

73.83003°

Altitude

499.728 km

Speed

7.614 km/s

True Right ascension

00h 06m 33s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

Latitude

Unknown

Longitude

Unknown

Altitude

Unknown

Speed

Unknown

Apparent Right ascension

Unknown

Apparent Declination

Unknown

Sunlit

N/A

Visualization observer readout

Local Sidereal Time

13:19:34

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

500.552 km

Perigee altitude

485.354 km

Semi-major axis

6,871.09 km

Eccentricity

0.00111

Inclination

97.6212°

RAAN

1.64°

Arg. of periapsis

95.1486°

True anomaly

264.97495°

Mean anomaly

265.1012°

Eccentric anomaly

265.03807°

Mean motion

3.8107 °/min

Orbital period

94.47 mins

BSTAR

0.00014508

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Other satellites on launch #57 in the year 2022 (2022-05-25 UTC)

LEMUR 2 TENNYSONLILY, 52732 (Decayed)

HAWK-5B, 52756

HAWK-5A, 52757

ICEYE-X19, 52758 (Decayed)

ICEYE-X20, 52759

ION SCV-006, 52761

ICEYE-X17, 52762 (Decayed)

SHERPA-AC1, 52763

NUSAT-29 (EDITH CLARKE), 52764

ARMSAT1 URDANETA, 52765

CELESTIS 21/VARISAT 1C, 52766 (Decayed)

CNCE4, 52767 (Decayed)

CNCE5, 52768 (Decayed)

LEMUR 2 MIMI1307, 52769 (Decayed)

VIGORIDE 3 Visibility forecast

Observer location: undefined°, undefined°
Set Observer location

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	2025-08-22 08:03:06.281Z	124.047° SE	2025-08-22 08:05:06.281Z	84.784° E	23.957°	2025-08-22 08:08:06.281Z	17.055° NNE
5 mins	2025-08-22 21:06:06.281Z	42.266° NE	2025-08-22 21:08:06.281Z	99.954° ESE	31.07°	2025-08-22 21:11:06.281Z	165.449° S