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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 src="https://www.satcat.com/sats-embedded/55056?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

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 (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, 3.3 m

Radar Cross Section

1.548 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 10 hours ago

TLE from 10 hours ago

0 VIGORIDE 5
1 55056U 23001AZ  26227.74902149  .00055544  00000-0  51089-3 0  9991
2 55056  97.3178 301.4787 0003573 288.7438  71.3435 15.67510743201977

Epoch: 2026-08-15T17:58Z

TLE epoch observation values (Epoch: 2026-08-15T17:58:35.456Z)

Latitude

-0.00005°

Longitude

67.67554°

Altitude

368.414 km

Speed

7.689 km/s

True Right ascension

20h 05m 54s

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

18:37:58

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

365.335 km

Perigee altitude

360.518 km

Semi-major axis

6,741.064 km

Eccentricity

0.00036

Inclination

97.3178°

RAAN

301.4787°

Arg. of periapsis

288.7438°

True anomaly

71.3823°

Mean anomaly

71.3435°

Eccentric anomaly

71.3629°

Mean motion

3.92148 °/min

Orbital period

91.8 mins

BSTAR

0.00051089

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

FLOCK 4Y 21, 55077 (Decayed)

ASTROCAST-0404, 55112

LEMUR 2 DISCLAIMER, 55014 (Decayed)

FLOCK 4Y 11, 55043 (Decayed)

FLOCK 4Y 16, 55040 (Decayed)

FLOCK 4Y 24, 55020 (Decayed)

FLOCK 4Y 34, 55082 (Decayed)

ASTROCAST-0403, 55111

EOSSAT-1, 55053

LYNK TOWER 4, 55034

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	2026-08-16 04:50:10.280Z	150.611° SSE	2026-08-16 04:52:10.280Z	101.973° ESE	36.912°	2026-08-16 04:55:10.280Z	358.714° N

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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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