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: 1 day ago
TLE from 1 day ago
0 VINDLER 2.2
1 68484U 26067BW 26259.31249443 .00001480 00000-0 15059-3 0 9991
2 68484 97.7622 217.1182 0002959 60.4594 299.6920 14.92241480 25368Epoch: 2026-09-16T07:29Z
TLE epoch observation values (Epoch: 2026-09-16T07:29:59.518Z)
Latitude
-0.00001°
Longitude
109.35432°
Altitude
592.969 km
Speed
7.564 km/s
True Right ascension
14h 28m 28s
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
02:59:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
590.028 km
Perigee altitude
585.905 km
Semi-major axis
6,966.104 km
Eccentricity
0.0003
Inclination
97.7622°
RAAN
217.1182°
Arg. of periapsis
60.4594°
True anomaly
299.66254°
Mean anomaly
299.692°
Eccentric anomaly
299.67727°
Mean motion
3.733 °/min
Orbital period
96.44 mins
BSTAR
0.00015059
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-09-17 11:25:41.573Z | 324.304° NNW | 2026-09-17 11:27:41.573Z | 294.952° NW | 13.793° | 2026-09-17 11:29:41.573Z | 265.712° W |
| 6 mins | 2026-09-17 20:39:41.573Z | 122.268° SE | 2026-09-17 20:41:41.573Z | 84.349° E | 29.924° | 2026-09-17 20:45:41.573Z | 9.776° NNE |
| 5 mins | 2026-09-17 22:15:41.573Z | 229.652° WSW | 2026-09-17 22:17:41.573Z | 265.045° W | 20.122° | 2026-09-17 22:20:41.573Z | 312.843° NW |
| 6 mins | 2026-09-18 09:58:41.573Z | 27.26° NE | 2026-09-18 10:00:41.573Z | 85.414° E | 62.046° | 2026-09-18 10:04:41.573Z | 181.903° SSW |
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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