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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55056 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Momentus
Mission
Operational Commercial Technology
Bus & Motor
VIGORIDE, AOCS
Mass
363 kg wet, 292 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 3.3 m
Radar Cross Section
1.548 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 VIGORIDE 5
1 55056U 23001AZ 26068.71571307 .00051437 00000-0 81503-3 0 9990
2 55056 97.3326 137.4712 0005037 140.3032 219.8591 15.53238104177187Epoch: 2026-03-09T17:10Z
TLE epoch observation values (Epoch: 2026-03-09T17:10:37.609Z)
Latitude
0.00002°
Longitude
72.40982°
Altitude
413.041 km
Speed
7.662 km/s
True Right ascension
09h 09m 53s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
06:36:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
407.614 km
Perigee altitude
400.781 km
Semi-major axis
6,782.335 km
Eccentricity
0.0005
Inclination
97.3326°
RAAN
137.4712°
Arg. of periapsis
140.3032°
True anomaly
219.82213°
Mean anomaly
219.8591°
Eccentric anomaly
219.84061°
Mean motion
3.88575 °/min
Orbital period
92.65 mins
BSTAR
0.00081503
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Other satellites on launch #1 in the year 2023 (2023-01-03 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.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 | 2026-03-10 04:08:00.254Z | 139.002° SSE | 2026-03-10 04:11:00.254Z | 58.917° ENE | 28.72° | 2026-03-10 04:13:00.254Z | 11.448° NNE |
| 4 mins | 2026-03-10 16:57:00.254Z | 52.646° ENE | 2026-03-10 16:58:00.254Z | 84.043° E | 27.083° | 2026-03-10 17:01:00.254Z | 162.344° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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