VINDLER 2.3, 68486
Orbit data source: Space-Track
VINDLER 2.3, 68486 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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68486 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: 13 hours ago
TLE from 13 hours ago
0 VINDLER 2.3
1 68486U 26067BY 26193.86235323 .00000710 00000-0 75408-4 0 9992
2 68486 97.7589 151.7200 0000989 114.5197 245.6125 14.92058525 15551Epoch: 2026-07-12T20:41Z
TLE epoch observation values (Epoch: 2026-07-12T20:41:47.319Z)
Latitude
-0.00001°
Longitude
-89.48229°
Altitude
594.845 km
Speed
7.562 km/s
True Right ascension
10h 06m 52s
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
22:24:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
589.225 km
Perigee altitude
587.847 km
Semi-major axis
6,966.673 km
Eccentricity
0.0001
Inclination
97.7589°
RAAN
151.72°
Arg. of periapsis
114.5197°
True anomaly
245.60218°
Mean anomaly
245.6125°
Eccentric anomaly
245.60734°
Mean motion
3.73254 °/min
Orbital period
96.45 mins
BSTAR
0.000075408
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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 2.3 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-07-13 10:07:40.766Z | 11.589° NNE | 2026-07-13 10:11:40.766Z | 333.976° NNW | 44.907° | 2026-07-13 10:15:40.766Z | 194.716° SSW |
| 6 mins | 2026-07-13 20:58:40.766Z | 146.661° SSE | 2026-07-13 21:01:40.766Z | 53.282° ENE | 39.165° | 2026-07-13 21:04:40.766Z | 358.843° 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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