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VIGORIDE 5, 55056

Orbit data source: Space-Track

VIGORIDE 5, 55056 is a payload satellite owned by Momentus (US) in SSO that was launched on Tue, 03 Jan 2023 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/55056?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

55056, 2023-001AZ

Orbit

SSO

Country

US

Related business

Momentus Space (US)

Manufacturer

Momentus

Mission

Operational Commercial Technology

Bus & Motor

VIGORIDE, AOCS

Mass

363 kg wet, 292 kg dry

Launch date (UTC)

2023-01-03 (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
Last TLE update: 6 hours ago

TLE from 6 hours ago

0 VIGORIDE 5
1 55056U 23001AZ  26166.46379772  .00051885  00000-0  61283-3 0  9993
2 55056  97.3224 237.8962 0006400 155.8597 204.2962 15.61144567192396

Epoch: 2026-06-15T11:07Z

TLE epoch observation values (Epoch: 2026-06-15T11:07:52.123Z)

Latitude

0.00004°

Longitude

167.1792°

Altitude

391.444 km

Speed

7.673 km/s

True Right ascension

15h 51m 35s

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

03:54:36

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

385.583 km

Perigee altitude

376.931 km

Semi-major axis

6,759.394 km

Eccentricity

0.00064

Inclination

97.3224°

RAAN

237.8962°

Arg. of periapsis

155.8597°

True anomaly

204.26605°

Mean anomaly

204.2962°

Eccentric anomaly

204.28112°

Mean motion

3.90554 °/min

Orbital period

92.18 mins

BSTAR

0.00061283

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Other satellites on launch #1 in the year 2023 (2023-01-03 UTC)

FLOCK 4Y 20, 55063 (Decayed)

AAC-AIS-SAT-1, 55107

LYNK TOWER 4, 55034

ICEYE-X21, 55049

EOSSAT-1, 55053

ASTROCAST-0403, 55111

SPACEBEE-157, 55102 (Decayed)

SPACEBEE-166, 55092 (Decayed)

LEMUR 2 MMOLO, 55038 (Decayed)

SPACEBEE-156, 55099 (Decayed)

FLOCK 4Y 2, 55074 (Decayed)

FLOCK 4Y 23, 55080 (Decayed)

CONTINUUM-1, 55045

SHARJAHSAT-1, 55104

Did you know?

You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.

Click here to try in Sandbox

VIGORIDE 5 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	2026-06-15 17:50:03.664Z	2.572° NNE	2026-06-15 17:53:03.664Z	251.665° W	38.349°	2026-06-15 17:55:03.664Z	206.994° SW

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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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Check out VIGORIDE 5, 55056 on other resources

View VIGORIDE 5, 55056 on NASA - NSSDCA Website

View VIGORIDE 5, 55056 on Heavens-Above

View VIGORIDE 5, 55056 on Keep Track

View VIGORIDE 5, 55056 on Celestrak

View VIGORIDE 5, 55056 on Gunter's Space Page

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

Documentation

Go to standalone docs website

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