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: 2 days ago
TLE from 2 days ago
0 VIGORIDE 7
1 68473U 26067BK 26258.85639161 .00007052 00000-0 29647-3 0 9996
2 68473 97.4640 216.8900 0009086 180.3592 179.7640 15.23690037 25734Epoch: 2026-09-15T20:33Z
TLE epoch observation values (Epoch: 2026-09-15T20:33:12.235Z)
Latitude
-0°
Longitude
-86.22731°
Altitude
504.062 km
Speed
7.609 km/s
True Right ascension
14h 27m 33s
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
02:02:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
497.927 km
Perigee altitude
485.443 km
Semi-major axis
6,869.822 km
Eccentricity
0.00091
Inclination
97.464°
RAAN
216.89°
Arg. of periapsis
180.3592°
True anomaly
179.76443°
Mean anomaly
179.764°
Eccentric anomaly
179.76421°
Mean motion
3.81175 °/min
Orbital period
94.44 mins
BSTAR
0.00029647
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-17 09:22:34.589Z | 45.491° ENE | 2026-09-17 09:25:34.589Z | 100.992° ESE | 19.938° | 2026-09-17 09:27:34.589Z | 138.545° SSE |
| 4 mins | 2026-09-17 10:57:34.589Z | 320.81° NNW | 2026-09-17 10:58:34.589Z | 297.857° NW | 22.512° | 2026-09-17 11:01:34.589Z | 238.746° WSW |
| 5 mins | 2026-09-17 21:33:34.589Z | 187.868° SSW | 2026-09-17 21:35:34.589Z | 291.33° WNW | 58.346° | 2026-09-17 21:38:34.589Z | 340.414° N |
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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