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: 23 hours ago
TLE from 23 hours ago
0 VINDLER 2.3
1 68486U 26067BY 26217.46809782 .00000882 00000-0 92286-4 0 9994
2 68486 97.7611 174.9729 0002186 110.8537 249.2917 14.92116729 19079Epoch: 2026-08-05T11:14Z
TLE epoch observation values (Epoch: 2026-08-05T11:14:03.651Z)
Latitude
0.00005°
Longitude
52.43561°
Altitude
594.918 km
Speed
7.562 km/s
True Right ascension
11h 39m 53s
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
23:57:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
589.878 km
Perigee altitude
586.832 km
Semi-major axis
6,966.492 km
Eccentricity
0.00022
Inclination
97.7611°
RAAN
174.9729°
Arg. of periapsis
110.8537°
True anomaly
249.26827°
Mean anomaly
249.2917°
Eccentric anomaly
249.27999°
Mean motion
3.73269 °/min
Orbital period
96.45 mins
BSTAR
0.000092286
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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 | 2026-08-06 10:19:56.584Z | 3.676° NNE | 2026-08-06 10:22:56.584Z | 310.629° NW | 41.112° | 2026-08-06 10:26:56.584Z | 205.252° SW |
| 7 mins | 2026-08-06 21:09:56.584Z | 160.488° S | 2026-08-06 21:12:56.584Z | 51.394° ENE | 44.274° | 2026-08-06 21:16:56.584Z | 350.489° 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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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