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, 0.5 m
Radar Cross Section
0.480 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 FGN-100-D2
1 66299U 25248G 26241.99140384 .00003871 00000-0 18397-3 0 9996
2 66299 45.4011 85.2245 0003568 114.3541 245.7719 15.21002641 45754Epoch: 2026-08-29T23:47Z
TLE epoch observation values (Epoch: 2026-08-29T23:47:37.291Z)
Latitude
0.00001°
Longitude
110.12573°
Altitude
503.866 km
Speed
7.613 km/s
True Right ascension
05h 40m 53s
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
19:43:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
506.808 km
Perigee altitude
501.897 km
Semi-major axis
6,882.489 km
Eccentricity
0.00036
Inclination
45.4011°
RAAN
85.2245°
Arg. of periapsis
114.3541°
True anomaly
245.73462°
Mean anomaly
245.7719°
Eccentric anomaly
245.75326°
Mean motion
3.80124 °/min
Orbital period
94.71 mins
BSTAR
0.00018397
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-08-31 15:22:10.662Z | 178.609° S | 2026-08-31 15:24:10.662Z | 146.083° SSE | 16.36° | 2026-08-31 15:26:10.662Z | 108.988° ESE |
| 5 mins | 2026-08-31 17:01:10.662Z | 242.262° WSW | 2026-08-31 17:03:10.662Z | 219.911° SW | 44.716° | 2026-08-31 17:06:10.662Z | 66.197° ENE |
| 5 mins | 2026-08-31 18:41:10.662Z | 303.108° NW | 2026-08-31 18:43:10.662Z | 8.305° NNE | 30.877° | 2026-08-31 18:46:10.662Z | 60.977° ENE |
| 5 mins | 2026-08-31 20:20:10.662Z | 308.813° NW | 2026-08-31 20:22:10.662Z | 357.302° N | 33.272° | 2026-08-31 20:25:10.662Z | 77.647° E |
| 6 mins | 2026-08-31 21:59:10.662Z | 287.085° WNW | 2026-08-31 22:02:10.662Z | 176.023° S | 40.932° | 2026-08-31 22:05:10.662Z | 128.577° SE |
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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