FGN-100-D2, 66299
Orbit data source: Space-Track
FGN-100-D2, 66299 is a Turkish payload satellite in LEO that was launched on Sun, 02 Nov 2025 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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
Orbit
Country
TR / TURKRelated business
Manufacturer
FERG
Mission
Operational Commercial Navigation
Bus & Motor
FGN-100, Unknown motor
Mass
102 kg wet, 102 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: 19 hours ago
TLE from 19 hours ago
0 FGN-100-D2
1 66299U 25248G 26295.05382161 .00003835 00000-0 18037-3 0 9994
2 66299 45.3997 160.4021 0003377 28.9025 331.2048 15.21389525 53832Epoch: 2026-10-22T01:17Z
TLE epoch observation values (Epoch: 2026-10-22T01:17:30.187Z)
Latitude
-0.00002°
Longitude
110.53206°
Altitude
499.656 km
Speed
7.617 km/s
True Right ascension
10h 41m 36s
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
15:28:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
505.51 km
Perigee altitude
500.862 km
Semi-major axis
6,881.323 km
Eccentricity
0.00034
Inclination
45.3997°
RAAN
160.4021°
Arg. of periapsis
28.9025°
True anomaly
331.18615°
Mean anomaly
331.2048°
Eccentric anomaly
331.19548°
Mean motion
3.8022 °/min
Orbital period
94.68 mins
BSTAR
0.00018037
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Other satellites on launch #248 in the year 2025 (2025-11-02 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-D2 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-10-22 20:30:19.179Z | 284.61° WNW | 2026-10-22 20:33:19.179Z | 347.923° N | 38.526° | 2026-10-22 20:36:19.179Z | 56.798° ENE |
| 5 mins | 2026-10-22 22:11:19.179Z | 316.307° NNW | 2026-10-22 22:13:19.179Z | 20.351° NNE | 39.843° | 2026-10-22 22:16:19.179Z | 79.164° E |
| 5 mins | 2026-10-22 23:50:19.179Z | 287.642° WNW | 2026-10-22 23:52:19.179Z | 226.704° WSW | 70.763° | 2026-10-22 23:55:19.179Z | 125.936° SE |
| 6 mins | 2026-10-23 18:30:19.179Z | 241.049° WSW | 2026-10-23 18:32:19.179Z | 207.172° SW | 81.942° | 2026-10-23 18:36:19.179Z | 66.05° ENE |
| 6 mins | 2026-10-23 20:09:19.179Z | 290.116° WNW | 2026-10-23 20:12:19.179Z | 9.648° NNE | 36.536° | 2026-10-23 20:15:19.179Z | 60.726° ENE |
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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