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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: 13 hours ago

TLE from 13 hours ago

0 VIGORIDE 5
1 55056U 23001AZ  25340.64425075  .00036235  00000-0  74656-3 0  9994
2 55056  97.3490  42.7778 0006186  80.7366 279.4583 15.45810993162777

Epoch: 2025-12-06T15:27Z

TLE epoch observation values (Epoch: 2025-12-06T15:27:43.264Z)

Latitude

-0.00001°

Longitude

95.1785°

Altitude

431.433 km

Speed

7.653 km/s

True Right ascension

02h 51m 06s

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

02:15:33

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

430.134 km

Perigee altitude

421.716 km

Semi-major axis

6,804.062 km

Eccentricity

0.00062

Inclination

97.349°

RAAN

42.7778°

Arg. of periapsis

80.7366°

True anomaly

279.38837°

Mean anomaly

279.4583°

Eccentric anomaly

279.42334°

Mean motion

3.86715 °/min

Orbital period

93.09 mins

BSTAR

0.00074656

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

FUTURA-SM1, 55105 (Decayed)

FLOCK 4Y 32, 55021 (Decayed)

KUWAITSAT-1, 55103

BIRKELAND, 55015

FLOCK 4Y 29, 55030 (Decayed)

FLOCK 4Y 17, 55031 (Decayed)

FLOCK 4Y 4, 55055 (Decayed)

FLOCK 4Y 16, 55040 (Decayed)

SPACEBEE-162, 55095 (Decayed)

STERNULA-1, 55044 (Decayed)

NSL-2, 55067 (Decayed)

LEMUR 2 FUENTETAJA-01, 55088 (Decayed)

FLOCK 4Y 36, 55078 (Decayed)

FLOCK 4Y 2, 55074 (Decayed)

SPACEBEE-166, 55092 (Decayed)

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.

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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	2025-12-07 16:53:15.944Z	31.577° NE	2025-12-07 16:55:15.944Z	90.029° ESE	35.134°	2025-12-07 16:58:15.944Z	172.694° S

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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

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