VIGORIDE 7, 68473
Orbit data source: Space-Track
VIGORIDE 7, 68473 is an American payload satellite 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
None
Manufacturer
Unknown
Mission
Operational spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 1.1 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 VIGORIDE 7
1 68473U 26067BK 26131.62261219 .00008919 00000-0 43403-3 0 9995
2 68473 97.4515 90.6300 0003635 143.1543 216.9942 15.18612743 6374Epoch: 2026-05-11T14:56Z
TLE epoch observation values (Epoch: 2026-05-11T14:56:33.693Z)
Latitude
0.00003°
Longitude
-2.91909°
Altitude
515.12 km
Speed
7.605 km/s
True Right ascension
06h 02m 31s
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
18:19:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.505 km
Perigee altitude
504.499 km
Semi-major axis
6,885.139 km
Eccentricity
0.00036
Inclination
97.4515°
RAAN
90.63°
Arg. of periapsis
143.1543°
True anomaly
216.96914°
Mean anomaly
216.9942°
Eccentric anomaly
216.98167°
Mean motion
3.79904 °/min
Orbital period
94.76 mins
BSTAR
0.00043403
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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 | 2026-05-12 10:28:33.132Z | 357.249° N | 2026-05-12 10:31:33.132Z | 292.556° NW | 35.492° | 2026-05-12 10:34:33.132Z | 215.998° SW |
| 6 mins | 2026-05-12 21:07:33.132Z | 154.202° SSE | 2026-05-12 21:10:33.132Z | 31.575° NE | 40.059° | 2026-05-12 21:13:33.132Z | 354.481° N |
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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