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 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 2.3
1 68486U 26067BY 26171.39578634 .00001132 00000-0 11720-3 0 9996
2 68486 97.7580 129.5960 0001217 52.3633 307.7696 14.91991260 12200Epoch: 2026-06-20T09:29Z
TLE epoch observation values (Epoch: 2026-06-20T09:29:55.939Z)
Latitude
-0.00006°
Longitude
78.50191°
Altitude
594.25 km
Speed
7.563 km/s
True Right ascension
08h 38m 23s
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
12:25:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
589.594 km
Perigee altitude
587.898 km
Semi-major axis
6,966.883 km
Eccentricity
0.00012
Inclination
97.758°
RAAN
129.596°
Arg. of periapsis
52.3633°
True anomaly
307.75858°
Mean anomaly
307.7696°
Eccentric anomaly
307.76409°
Mean motion
3.73238 °/min
Orbital period
96.45 mins
BSTAR
0.0001172
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-22 10:20:48.148Z | 3.939° NNE | 2026-06-22 10:24:48.148Z | 256.623° W | 40.336° | 2026-06-22 10:27:48.148Z | 207.134° SW |
| 6 mins | 2026-06-22 21:11:48.148Z | 160.603° S | 2026-06-22 21:13:48.148Z | 124.637° SE | 44.143° | 2026-06-22 21:17:48.148Z | 350.153° 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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