VINDLER 2.2, 68484
Orbit data source: Space-Track
VINDLER 2.2, 68484 is a payload satellite owned by Sierra Nevada (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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68484 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Muon Space
Mission
Operational Commercial Sigint
Bus & Motor
MUON HALO, Unknown motor
Mass
~130 kg wet, ~130 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 2.5 m
Radar Cross Section
2.173 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 VINDLER 2.2
1 68484U 26067BW 26263.20165992 .00000731 00000-0 77124-4 0 9990
2 68484 97.7631 220.9512 0002837 54.1685 305.9797 14.92247186 25949Epoch: 2026-09-20T04:50Z
TLE epoch observation values (Epoch: 2026-09-20T04:50:23.417Z)
Latitude
-0.00003°
Longitude
149.2544°
Altitude
592.811 km
Speed
7.564 km/s
True Right ascension
14h 43m 48s
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
09:41:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
589.925 km
Perigee altitude
585.972 km
Semi-major axis
6,966.086 km
Eccentricity
0.00028
Inclination
97.7631°
RAAN
220.9512°
Arg. of periapsis
54.1685°
True anomaly
305.95339°
Mean anomaly
305.9797°
Eccentric anomaly
305.96654°
Mean motion
3.73302 °/min
Orbital period
96.44 mins
BSTAR
0.000077124
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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.VINDLER 2.2 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-09-20 21:03:38.302Z | 151.59° SSE | 2026-09-20 21:06:38.302Z | 95.732° ESE | 57.951° | 2026-09-20 21:10:38.302Z | 356.387° N |
| 8 mins | 2026-09-21 10:21:38.302Z | 6.133° NNE | 2026-09-21 10:25:38.302Z | 293.066° NW | 65.182° | 2026-09-21 10:29:38.302Z | 203.822° SW |
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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