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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68464 intel report (Beta)
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Identifier
Orbit
Country
TR / TURKRelated business
Manufacturer
FERG
Mission
Operational Commercial Navigation
Bus & Motor
FGN-100, Unknown motor
Mass
113 kg wet, 113 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.6 m
Radar Cross Section
0.480 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 FGN-100-D3
1 68464U 26067BA 26260.19094376 .00003433 00000-0 17031-3 0 9992
2 68464 97.4623 217.2170 0004682 111.4797 248.6937 15.18381420 25897Epoch: 2026-09-17T04:34Z
TLE epoch observation values (Epoch: 2026-09-17T04:34:57.540Z)
Latitude
-0.00002°
Longitude
152.34552°
Altitude
514.992 km
Speed
7.606 km/s
True Right ascension
14h 28m 52s
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
04:04:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
510.926 km
Perigee altitude
504.478 km
Semi-major axis
6,885.839 km
Eccentricity
0.00047
Inclination
97.4623°
RAAN
217.217°
Arg. of periapsis
111.4797°
True anomaly
248.64373°
Mean anomaly
248.6937°
Eccentric anomaly
248.66871°
Mean motion
3.79846 °/min
Orbital period
94.78 mins
BSTAR
0.00017031
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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.FGN-100-D3 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 20:32:33.327Z | 120.273° SE | 2026-09-17 20:35:33.327Z | 59.45° ENE | 23.393° | 2026-09-17 20:37:33.327Z | 22.165° NNE |
| 4 mins | 2026-09-17 22:07:33.327Z | 233.862° WSW | 2026-09-17 22:08:33.327Z | 254.093° W | 20.044° | 2026-09-17 22:11:33.327Z | 311.549° NW |
| 5 mins | 2026-09-18 09:38:33.327Z | 49.824° ENE | 2026-09-18 09:40:33.327Z | 112.217° ESE | 34.297° | 2026-09-18 09:43:33.327Z | 165.101° S |
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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