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VINDLER 2.1, 68488

Orbit data source: Space-Track

VINDLER 2.1, 68488 is a payload satellite owned by NearSpaceLaunch (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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Identifier
68488, 2026-067CA
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
NearSpaceLaunch
Mission
Operational Commercial Sigint
Bus & Motor
THINSAT 0.5U, Unknown motor
Mass
0.5 kg wet, 0.5 kg dry
Launch date (UTC)
2026-03-30 (4 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 2.5 m
Radar Cross Section
2.173 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 10 hours ago

TLE from 10 hours ago
0 VINDLER 2.1
1 68488U 26067CA  26218.13903299  .00000747  00000-0  79014-4 0  9993
2 68488  97.7607 175.6257 0000946 129.5013 230.6290 14.92117582 19175
Epoch: 2026-08-06T03:20Z
TLE epoch observation values (Epoch: 2026-08-06T03:20:12.450Z)
Latitude
0.00001°
Longitude
170.89045°
Altitude
594.794 km
Speed
7.562 km/s
True Right ascension
11h 42m 30s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
02:58:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
589.011 km
Perigee altitude
587.693 km
Semi-major axis
6,966.489 km
Eccentricity
0.00009
Inclination
97.7607°
RAAN
175.6257°
Arg. of periapsis
129.5013°
True anomaly
230.62062°
Mean anomaly
230.629°
Eccentric anomaly
230.62481°
Mean motion
3.73269 °/min
Orbital period
96.45 mins
BSTAR
0.000079014
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