VINDLER 2.3, 68486
Orbit data source: Space-Track
VINDLER 2.3, 68486 is an American payload satellite 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
None
Manufacturer
Unknown
Mission
Operational spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 1.1 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 VINDLER 2.3
1 68486U 26067BY 26127.19691139 .00001241 00000-0 12845-3 0 9991
2 68486 97.7559 86.0878 0002665 92.6868 267.4656 14.91838538 5619Epoch: 2026-05-07T04:43Z
TLE epoch observation values (Epoch: 2026-05-07T04:43:33.144Z)
Latitude
0.00001°
Longitude
150.15319°
Altitude
595.327 km
Speed
7.562 km/s
True Right ascension
05h 44m 21s
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
22:03:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
591.078 km
Perigee altitude
587.365 km
Semi-major axis
6,967.359 km
Eccentricity
0.00027
Inclination
97.7559°
RAAN
86.0878°
Arg. of periapsis
92.6868°
True anomaly
267.43509°
Mean anomaly
267.4656°
Eccentric anomaly
267.45035°
Mean motion
3.73199 °/min
Orbital period
96.46 mins
BSTAR
0.00012845
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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 | 2026-05-07 20:57:20.937Z | 147.545° SSE | 2026-05-07 21:00:20.937Z | 78.989° E | 39.106° | 2026-05-07 21:04:20.937Z | 357.458° N |
| 7 mins | 2026-05-08 10:16:20.937Z | 5.86° NNE | 2026-05-08 10:19:20.937Z | 289.753° WNW | 43.448° | 2026-05-08 10:23:20.937Z | 201.044° SSW |
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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