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, 1.4 m
Radar Cross Section
0.725 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 VIGORIDE 7
1 68473U 26067BK 26217.40911244 .00006052 00000-0 25927-3 0 9993
2 68473 97.4567 175.6874 0008733 351.3669 8.7416 15.23115101 19422Epoch: 2026-08-05T09:49Z
TLE epoch observation values (Epoch: 2026-08-05T09:49:07.314Z)
Latitude
-0.00005°
Longitude
74.443°
Altitude
493.609 km
Speed
7.621 km/s
True Right ascension
11h 42m 44s
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
10:50:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
499.416 km
Perigee altitude
487.414 km
Semi-major axis
6,871.552 km
Eccentricity
0.00087
Inclination
97.4567°
RAAN
175.6874°
Arg. of periapsis
351.3669°
True anomaly
8.75683°
Mean anomaly
8.7416°
Eccentric anomaly
8.74921°
Mean motion
3.81032 °/min
Orbital period
94.48 mins
BSTAR
0.00025927
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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 | 2026-08-05 20:58:48.138Z | 147.6° SSE | 2026-08-05 21:01:48.138Z | 93.267° ESE | 35.148° | 2026-08-05 21:04:48.138Z | 4.76° NNE |
| 5 mins | 2026-08-06 10:02:48.138Z | 20.993° NNE | 2026-08-06 10:04:48.138Z | 84.81° E | 43.264° | 2026-08-06 10:07:48.138Z | 184.499° SSW |
| 4 mins | 2026-08-06 20:39:48.138Z | 111.451° ESE | 2026-08-06 20:41:48.138Z | 62.081° ENE | 22.967° | 2026-08-06 20:43:48.138Z | 21.49° NNE |
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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