VIGORIDE 7, 68473
Orbit data source: Space-Track
VIGORIDE 7, 68473 is a payload satellite owned by Momentus (US) in SSO that was launched on Mon, 30 Mar 2026 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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68473 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, 3.3 m
Radar Cross Section
0.725 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 VIGORIDE 7
1 68473U 26067BK 26307.64238250 .00006430 00000-0 26546-3 0 9996
2 68473 97.4724 265.4781 0010236 31.1315 329.0527 15.24332353 33164Epoch: 2026-11-03T15:25Z
TLE epoch observation values (Epoch: 2026-11-03T15:25:01.848Z)
Latitude
0.00003°
Longitude
-8.68172°
Altitude
489.854 km
Speed
7.623 km/s
True Right ascension
17h 41m 54s
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
09:56:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
496.784 km
Perigee altitude
482.724 km
Semi-major axis
6,867.891 km
Eccentricity
0.00102
Inclination
97.4724°
RAAN
265.4781°
Arg. of periapsis
31.1315°
True anomaly
328.99231°
Mean anomaly
329.0527°
Eccentric anomaly
329.02251°
Mean motion
3.81336 °/min
Orbital period
94.4 mins
BSTAR
0.00026546
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Other satellites on launch #67 in the year 2026 (2026-03-30 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 7 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 | 2026-11-04 21:28:09.748Z | 172.608° S | 2026-11-04 21:31:09.748Z | 207.796° SW | 67.237° | 2026-11-04 21:34:09.748Z | 342.801° N |
| 6 mins | 2026-11-05 10:31:09.748Z | 356.068° N | 2026-11-05 10:34:09.748Z | 256.201° W | 46.545° | 2026-11-05 10:37:09.748Z | 209.666° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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