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FR 1

NORAD 1814 Payload LEO 1965-101A ● Active
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🛰️ Orbital Parameters
Perigee
652 km
Apogee
659 km
Inclination
75.9°
Period
97.8 min
Mean Motion
14.71821214 rev/day
TLE Epoch
2026-10-20 23:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude656 km
Orbital Velocity27,115 km/h
Velocity7.53 km/s
Orbital Period98 minutes
Orbits / Day14.72
Eccentricity0.0005
Semi-Major Axis7,027 km
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇫🇷 CNES (France)
Launch Date
1965-12-06
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1965-101A
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
FR 1 is an active satellite operated by CNES (France), launched on 1965-12-06 from Vandenberg Space Force Base, United States on the FR-1 launch. After more than 61 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Low Earth Orbit (LEO) at altitudes between 652 km and 659 km with an inclination of 75.9°. It travels at approximately 27,115 km/h (7.53 km/s), completing one full orbit every 98 minutes — that’s roughly 14.72 orbits per day. 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 ~10–25 years. Orbital Radar tracks FR 1 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
FR 1 orbits at an average altitude of 656 km in the mid-LEO band, where atmospheric drag is minimal but radiation exposure remains manageable. Objects at this altitude persist for decades to centuries, making debris mitigation critical. This regime is popular for remote sensing constellations and scientific instruments that need stable, long-duration orbits. Within ±50 km of FR 1’s average altitude, there are currently 855 active payloads and 1,182 tracked debris or rocket body fragments — notable neighbours include TERRA, AQUA, ONEWEB-0179. With an inclination of 75.9°, FR 1 passes over latitudes between 75.9°N and 75.9°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. France operates approximately 124 active satellites in total, of which 46 share a similar altitude band with FR 1.
❓ Frequently Asked Questions
FR 1 orbits in Low Earth Orbit (LEO) at altitudes between 652 km (perigee) and 659 km (apogee), with an average altitude of approximately 656 km. It completes one orbit every 98 minutes, travelling at approximately 27,115 km/h (16,848 mph).
FR 1 is operated by CNES (France). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 1814. You can track FR 1 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
FR 1 was launched on 1965-12-06 from Vandenberg Space Force Base, United States, 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: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks FR 1 (NORAD ID 1814) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). 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.
FR 1 travels at approximately 27,115 km/h (16,848 mph) — roughly 7.53 km/s. It completes 14.72 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.