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 spacecraft
Bus & Motor
MUON HALO, Unknown motor
Mass
~130 kg wet, ~130 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 1.2 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 VINDLER 2.2
1 68484U 26067BW 26171.41668980 -.00018853 00000-0 -15529-2 0 9991
2 68484 97.7666 130.3776 0002296 352.5135 327.4141 14.99078604 2948Epoch: 2026-06-20T10:00Z
TLE epoch observation values (Epoch: 2026-06-20T10:00:01.998Z)
Latitude
-39.91672°
Longitude
78.25387°
Altitude
583.705 km
Speed
7.568 km/s
True Right ascension
09h 07m 34s
True Declination
-39° 44' 36"
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
12:32:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
568.346 km
Perigee altitude
565.157 km
Semi-major axis
6,944.888 km
Eccentricity
0.00023
Inclination
97.7666°
RAAN
130.3776°
Arg. of periapsis
352.5135°
True anomaly
327.39993°
Mean anomaly
327.4141°
Eccentric anomaly
327.40701°
Mean motion
3.75012 °/min
Orbital period
96 mins
BSTAR
-0.0015529
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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 | 2026-06-22 09:13:54.218Z | 58.208° ENE | 2026-06-22 09:15:54.218Z | 92.721° ESE | 17.59° | 2026-06-22 09:17:54.218Z | 127.983° SE |
| 5 mins | 2026-06-22 10:48:54.218Z | 339.268° N | 2026-06-22 10:50:54.218Z | 295.781° NW | 27.514° | 2026-06-22 10:53:54.218Z | 232.586° WSW |
| 6 mins | 2026-06-22 21:34:54.218Z | 184.662° SSW | 2026-06-22 21:37:54.218Z | 264.19° W | 39.632° | 2026-06-22 21:40:54.218Z | 335.255° NNW |
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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