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: 10 hours ago
TLE from 10 hours ago
0 VIGORIDE 3
1 52760U 22057AE 26091.34347197 .00007020 00000-0 27214-3 0 9990
2 52760 97.6473 229.3857 0009245 41.9177 318.2767 15.26430277213437Epoch: 2026-04-01T08:14Z
TLE epoch observation values (Epoch: 2026-04-01T08:14:35.978Z)
Latitude
-0.00001°
Longitude
-83.97187°
Altitude
484.851 km
Speed
7.625 km/s
True Right ascension
15h 17m 32s
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
23:52:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
489.805 km
Perigee altitude
477.118 km
Semi-major axis
6,861.599 km
Eccentricity
0.00092
Inclination
97.6473°
RAAN
229.3857°
Arg. of periapsis
41.9177°
True anomaly
318.20613°
Mean anomaly
318.2767°
Eccentric anomaly
318.24142°
Mean motion
3.81861 °/min
Orbital period
94.28 mins
BSTAR
0.00027214
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-04-01 21:24:06.217Z | 42.814° NE | 2026-04-01 21:27:06.217Z | 110.194° ESE | 23.374° | 2026-04-01 21:29:06.217Z | 149.583° SSE |
| 5 mins | 2026-04-02 09:33:06.217Z | 196.302° SSW | 2026-04-02 09:35:06.217Z | 251.289° W | 34.222° | 2026-04-02 09:38:06.217Z | 330.599° NNW |
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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