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: 1 day ago
TLE from 1 day ago
0 VINDLER 2.1
1 68488U 26067CA 26262.33019029 .00000806 00000-0 84513-4 0 9999
2 68488 97.7662 219.1818 0002700 84.5894 275.5633 14.92242071 25763Epoch: 2026-09-19T07:55Z
TLE epoch observation values (Epoch: 2026-09-19T07:55:28.441Z)
Latitude
0°
Longitude
102.07302°
Altitude
593.806 km
Speed
7.563 km/s
True Right ascension
14h 36m 43s
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
08:43:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
589.846 km
Perigee altitude
586.084 km
Semi-major axis
6,966.102 km
Eccentricity
0.00027
Inclination
97.7662°
RAAN
219.1818°
Arg. of periapsis
84.5894°
True anomaly
275.53251°
Mean anomaly
275.5633°
Eccentric anomaly
275.5479°
Mean motion
3.733 °/min
Orbital period
96.44 mins
BSTAR
0.000084513
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-09-20 21:03:16.735Z | 156.958° SSE | 2026-09-20 21:07:16.735Z | 69.596° E | 66.843° | 2026-09-20 21:11:16.735Z | 353.486° N |
| 6 mins | 2026-09-21 10:23:16.735Z | 359.246° N | 2026-09-21 10:26:16.735Z | 267.357° W | 57.066° | 2026-09-21 10:29:16.735Z | 209.327° SW |
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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