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 26228.60006551 .00000481 00000-0 52834-4 0 9993
2 68484 97.7704 186.8267 0002849 112.7682 247.3838 14.92128740 20784Epoch: 2026-08-16T14:24Z
TLE epoch observation values (Epoch: 2026-08-16T14:24:05.660Z)
Latitude
-0.00001°
Longitude
5.80885°
Altitude
595.105 km
Speed
7.562 km/s
True Right ascension
12h 27m 18s
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
16:59:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
590.303 km
Perigee altitude
586.333 km
Semi-major axis
6,966.455 km
Eccentricity
0.00028
Inclination
97.7704°
RAAN
186.8267°
Arg. of periapsis
112.7682°
True anomaly
247.35367°
Mean anomaly
247.3838°
Eccentric anomaly
247.36873°
Mean motion
3.73272 °/min
Orbital period
96.44 mins
BSTAR
0.000052834
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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 | 2026-08-17 10:16:51.088Z | 8.204° NNE | 2026-08-17 10:19:51.088Z | 333.834° NNW | 43.072° | 2026-08-17 10:23:51.088Z | 199.381° SSW |
| 7 mins | 2026-08-17 21:06:51.088Z | 153.405° SSE | 2026-08-17 21:09:51.088Z | 69.142° E | 42.19° | 2026-08-17 21:13:51.088Z | 353.91° 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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