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, Unknown HBR
Radar Cross Section
0.480 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 FGN-100-D2
1 66299U 25248G 26171.17778161 .00002845 00000-0 14065-3 0 9996
2 66299 45.4008 105.0776 0004050 58.2516 301.8765 15.20480758 34970Epoch: 2026-06-20T04:16Z
TLE epoch observation values (Epoch: 2026-06-20T04:16:00.331Z)
Latitude
0.00002°
Longitude
132.6801°
Altitude
502.962 km
Speed
7.615 km/s
True Right ascension
07h 00m 18s
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
07:16:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
508.715 km
Perigee altitude
503.138 km
Semi-major axis
6,884.064 km
Eccentricity
0.00041
Inclination
45.4008°
RAAN
105.0776°
Arg. of periapsis
58.2516°
True anomaly
301.83708°
Mean anomaly
301.8765°
Eccentric anomaly
301.85679°
Mean motion
3.79993 °/min
Orbital period
94.74 mins
BSTAR
0.00014065
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-20 21:46:41.355Z | 182.854° SSW | 2026-06-20 21:49:41.355Z | 131.321° SE | 17.028° | 2026-06-20 21:51:41.355Z | 98.415° ESE |
| 6 mins | 2026-06-20 23:25:41.355Z | 244.332° WSW | 2026-06-20 23:27:41.355Z | 244.055° WSW | 42.875° | 2026-06-20 23:31:41.355Z | 65.557° ENE |
| 5 mins | 2026-06-21 01:05:41.355Z | 298.298° NW | 2026-06-21 01:07:41.355Z | 354.506° N | 31.352° | 2026-06-21 01:10:41.355Z | 58.785° ENE |
| 5 mins | 2026-06-21 02:45:41.355Z | 316.696° NNW | 2026-06-21 02:47:41.355Z | 26.157° NE | 33.713° | 2026-06-21 02:50:41.355Z | 82.899° E |
| 5 mins | 2026-06-21 04:24:41.355Z | 282.582° WNW | 2026-06-21 04:26:41.355Z | 214.861° SW | 41.286° | 2026-06-21 04:29:41.355Z | 131.617° SE |
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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