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: 2 days ago
TLE from 2 days ago
0 VINDLER 2.1
1 68488U 26067CA 26258.64215969 .00001149 00000-0 11819-3 0 9998
2 68488 97.7668 215.5455 0002807 92.6935 267.4606 14.92224726 25217Epoch: 2026-09-15T15:24Z
TLE epoch observation values (Epoch: 2026-09-15T15:24:42.597Z)
Latitude
0.00006°
Longitude
-10.23717°
Altitude
594.13 km
Speed
7.563 km/s
True Right ascension
14h 22m 10s
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
04:04:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
589.974 km
Perigee altitude
586.063 km
Semi-major axis
6,966.156 km
Eccentricity
0.00028
Inclination
97.7668°
RAAN
215.5455°
Arg. of periapsis
92.6935°
True anomaly
267.42847°
Mean anomaly
267.4606°
Eccentric anomaly
267.44453°
Mean motion
3.73296 °/min
Orbital period
96.44 mins
BSTAR
0.00011819
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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 | 2026-09-17 20:40:19.404Z | 121.442° SE | 2026-09-17 20:42:19.404Z | 75.309° E | 33.945° | 2026-09-17 20:45:19.404Z | 12.94° NNE |
| 4 mins | 2026-09-17 22:16:19.404Z | 236.336° WSW | 2026-09-17 22:18:19.404Z | 271.432° WNW | 18.155° | 2026-09-17 22:20:19.404Z | 303.63° NW |
| 7 mins | 2026-09-18 09:58:19.404Z | 20.09° NNE | 2026-09-18 10:01:19.404Z | 118.37° SE | 69.635° | 2026-09-18 10:05:19.404Z | 185.978° SSW |
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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