VINDLER 2.1, 68488
Orbit data source: Space-Track
VINDLER 2.1, 68488 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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68488 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 2.1
1 68488U 26067CA 26254.41764858 .00001110 00000-0 11445-3 0 9998
2 68488 97.7661 211.3800 0002776 96.9148 263.2387 14.92205015 24585Epoch: 2026-09-11T10:01Z
TLE epoch observation values (Epoch: 2026-09-11T10:01:24.837Z)
Latitude
0°
Longitude
70.58521°
Altitude
594.332 km
Speed
7.563 km/s
True Right ascension
14h 05m 31s
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
15:45:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
590.014 km
Perigee altitude
586.146 km
Semi-major axis
6,966.217 km
Eccentricity
0.00028
Inclination
97.7661°
RAAN
211.38°
Arg. of periapsis
96.9148°
True anomaly
263.20711°
Mean anomaly
263.2387°
Eccentric anomaly
263.22291°
Mean motion
3.73291 °/min
Orbital period
96.44 mins
BSTAR
0.00011445
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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 2.1 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-12 09:08:18.888Z | 49.645° ENE | 2026-09-12 09:11:18.888Z | 96.961° ESE | 18.548° | 2026-09-12 09:13:18.888Z | 130.062° SE |
| 6 mins | 2026-09-12 10:44:18.888Z | 342.227° N | 2026-09-12 10:46:18.888Z | 302.307° NW | 32.566° | 2026-09-12 10:50:18.888Z | 225.729° WSW |
| 7 mins | 2026-09-12 21:33:18.888Z | 186.102° SSW | 2026-09-12 21:36:18.888Z | 258.523° W | 54.214° | 2026-09-12 21:40:18.888Z | 337.843° N |
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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