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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Edit Public Description
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: 17 hours ago
TLE from 17 hours ago
0 VIGORIDE 3
1 52760U 22057AE 25348.90640950 .00004615 00000-0 18898-3 0 9994
2 52760 97.6340 119.6626 0010225 55.2360 304.9838 15.24781385197054Epoch: 2025-12-14T21:45Z
TLE epoch observation values (Epoch: 2025-12-14T21:45:13.780Z)
Latitude
-0.00006°
Longitude
69.54259°
Altitude
490.509 km
Speed
7.622 km/s
True Right ascension
07h 58m 39s
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
13:22:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
495.432 km
Perigee altitude
481.39 km
Semi-major axis
6,866.548 km
Eccentricity
0.00102
Inclination
97.634°
RAAN
119.6626°
Arg. of periapsis
55.236°
True anomaly
304.88773°
Mean anomaly
304.9838°
Eccentric anomaly
304.93577°
Mean motion
3.81448 °/min
Orbital period
94.38 mins
BSTAR
0.00018898
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Other satellites on launch #57 in the year 2022 (2022-05-25 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 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 | 2025-12-15 21:56:23.136Z | 4.5° NNE | 2025-12-15 21:59:23.136Z | 260.972° W | 42.052° | 2025-12-15 22:02:23.136Z | 202.895° SW |
| 5 mins | 2025-12-16 08:33:23.136Z | 129.223° SE | 2025-12-16 08:35:23.136Z | 57.291° ENE | 32.921° | 2025-12-16 08:38:23.136Z | 2.55° 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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