VIGORIDE 3, 52760
Orbit data source: Space-Track
VIGORIDE 3, 52760 is a payload satellite owned by Momentus (US) in SSO that was launched on Wed, 25 May 2022 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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52760 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Momentus
Mission
Operational Commercial Technology
Bus & Motor
VIGORIDE, AOCS
Mass
412 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: 2 days ago
TLE from 2 days ago
0 VIGORIDE 3
1 52760U 22057AE 26171.42702770 .00004548 00000-0 17276-3 0 9999
2 52760 97.6612 311.4869 0009702 110.5914 249.6366 15.27308098225653Epoch: 2026-06-20T10:14Z
TLE epoch observation values (Epoch: 2026-06-20T10:14:55.193Z)
Latitude
-0.00001°
Longitude
-110.88488°
Altitude
489.279 km
Speed
7.619 km/s
True Right ascension
20h 45m 56s
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
21:55:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
487.485 km
Perigee altitude
474.176 km
Semi-major axis
6,858.968 km
Eccentricity
0.00097
Inclination
97.6612°
RAAN
311.4869°
Arg. of periapsis
110.5914°
True anomaly
249.53242°
Mean anomaly
249.6366°
Eccentric anomaly
249.5845°
Mean motion
3.82081 °/min
Orbital period
94.22 mins
BSTAR
0.00017276
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Other satellites on launch #57 in the year 2022 (2022-05-25 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 3 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 | 2026-06-22 22:33:31.408Z | 357.479° N | 2026-06-22 22:36:31.408Z | 268.725° W | 36.367° | 2026-06-22 22:39:31.408Z | 211.101° SW |
| 4 mins | 2026-06-23 09:09:31.408Z | 138.757° SSE | 2026-06-23 09:11:31.408Z | 44.366° NE | 37.156° | 2026-06-23 09:13:31.408Z | 2.133° NNE |
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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