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FGN-100-D3, 68464

Orbit data source: Space-Track

FGN-100-D3, 68464 is a Turkish 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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Identifier
68464, 2026-067BA
Orbit
SSO
Country
Flag of TRTR / TURK
Related business
Manufacturer
FERG
Mission
Operational spacecraft
Bus & Motor
FGN-100, Unknown motor
Mass
113 kg wet, 113 kg dry
Launch date (UTC)
2026-03-30 (3 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 14.5 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 FGN-100-D3
1 68464U 26067BA  26171.40282676  .00003596  00000-0  18163-3 0  9996
2 68464  97.4520 129.7191 0005051  81.2415 278.9391 15.17712466 12427
Epoch: 2026-06-20T09:40Z
TLE epoch observation values (Epoch: 2026-06-20T09:40:04.232Z)
Latitude
0.00004°
Longitude
76.0835°
Altitude
515.303 km
Speed
7.606 km/s
True Right ascension
08h 38m 52s
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
13:39:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
513.206 km
Perigee altitude
506.248 km
Semi-major axis
6,887.864 km
Eccentricity
0.00051
Inclination
97.452°
RAAN
129.7191°
Arg. of periapsis
81.2415°
True anomaly
278.88192°
Mean anomaly
278.9391°
Eccentric anomaly
278.91051°
Mean motion
3.79679 °/min
Orbital period
94.82 mins
BSTAR
0.00018163
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