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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Edit Public Description
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: 16 hours ago
TLE from 16 hours ago
0 VIGORIDE 5
1 55056U 23001AZ 26022.46046178 .00045041 00000-0 81560-3 0 9992
2 55056 97.3414 90.3056 0002204 317.4061 42.7019 15.49518575170016Epoch: 2026-01-22T11:03Z
TLE epoch observation values (Epoch: 2026-01-22T11:03:03.897Z)
Latitude
-0.00005°
Longitude
162.72606°
Altitude
420.165 km
Speed
7.66 km/s
True Right ascension
06h 01m 13s
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
03:57:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
416.554 km
Perigee altitude
413.56 km
Semi-major axis
6,793.194 km
Eccentricity
0.00022
Inclination
97.3414°
RAAN
90.3056°
Arg. of periapsis
317.4061°
True anomaly
42.71903°
Mean anomaly
42.7019°
Eccentric anomaly
42.71047°
Mean motion
3.87643 °/min
Orbital period
92.87 mins
BSTAR
0.0008156
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Other satellites on launch #1 in the year 2023 (2023-01-03 UTC)
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.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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-01-23 04:13:27.709Z | 153.288° SSE | 2026-01-23 04:16:27.709Z | 78.942° E | 38.992° | 2026-01-23 04:19:27.709Z | 358.113° N |
| 4 mins | 2026-01-23 17:04:27.709Z | 31.954° NE | 2026-01-23 17:06:27.709Z | 132.655° SE | 37.201° | 2026-01-23 17:08:27.709Z | 175.775° 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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