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FGN-100-D3

NORAD 68464 Payload LEO 2026-067BA ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
509 km
Apogee
516 km
Inclination
97.5°
Period
94.9 min
Mean Motion
15.17703028 rev/day
TLE Epoch
2026-06-19 03:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude513 km
Orbital Velocity27,395 km/h
Velocity7.61 km/s
Orbital Period95 minutes
Orbits / Day15.18
Eccentricity0.0005
Semi-Major Axis6,884 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
Turkey
Launch Date
2026-03-30
Launch Site
Vandenberg SFB, California
Int'l Designator
2026-067BA
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
FGN-100-D3 is an active satellite operated by Turkey, launched on 2026-03-30 from Vandenberg SFB, California. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Low Earth Orbit (LEO) at altitudes between 509 km and 516 km with an inclination of 97.5°. It travels at approximately 27,395 km/h (7.61 km/s), completing one full orbit every 95 minutes — that’s roughly 15.18 orbits per day. Its near-polar, sun-synchronous orbit means it passes over any given point on Earth at approximately the same local solar time, ideal for consistent Earth observation lighting conditions. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~3–10 years. Orbital Radar tracks FGN-100-D3 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
FGN-100-D3 orbits at an average altitude of 513 km in a sun-synchronous orbit (SSO), a specialised subset of LEO where the orbital plane precesses to maintain a constant angle relative to the Sun. This provides consistent lighting conditions on every pass — essential for Earth observation, weather monitoring and environmental science. Within ±50 km of FGN-100-D3’s average altitude, there are currently 8,917 active payloads and 266 tracked debris or rocket body fragments — notable neighbours include STARLINK-1017, STARLINK-1039, STARLINK-1184. This makes it one of the more crowded altitude bands, containing roughly 51.2% of all active satellites. With an inclination of 97.5°, FGN-100-D3 passes over latitudes between 97.5°N and 97.5°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. Turkey operates approximately 41 active satellites in total, of which 19 share a similar altitude band with FGN-100-D3.
❓ Frequently Asked Questions
FGN-100-D3 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 513 km altitude. Its 97.5° inclination causes the orbital plane to precess at exactly the rate of the Earth’s revolution around the Sun, so the satellite crosses each latitude at a consistent local solar time. It completes one orbit every 95 minutes, travelling at 27,395 km/h.
FGN-100-D3 is operated by Turkey. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 68464. You can track FGN-100-D3 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
FGN-100-D3 was launched on 2026-03-30 from Vandenberg SFB, California, primarily used for polar and sun-synchronous orbit launches due to its southward ocean trajectory from California. At its current altitude, the estimated remaining orbital lifetime is: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks FGN-100-D3 (NORAD ID 68464) using the latest TLE (two-line element set) data from Space-Track and CelesTrak. Open the live tracker to see its current position, altitude, speed and orbital path updated in real time. You can also browse the satellite directory to find other tracked objects.
FGN-100-D3 travels at approximately 27,395 km/h (17,022 mph) — roughly 7.61 km/s. It completes 15.18 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.