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FR 1, 1814

Orbit data source: Space-Track

FR 1, 1814 is a payload satellite owned by CNES (FR) in LEO that was launched on Mon, 06 Dec 1965 UTC via an SCOUT X-4 launch vehicle from the Air Force Western Test Range (AFWTR). 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
1814, 1965-101A
Orbit
LEO
Country
Flag of FRFR
Related business
Manufacturer
Nord
Mission
Civil Science
Bus & Motor
FR, Unknown motor
Mass
62 kg wet, 62 kg dry
Launch date (UTC)
1965-12-06 (60 years ago)
Launch vehicle
SCOUT X-4
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Poly + 4 Ant, 2.1 m
Radar Cross Section
1.303 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 11 hours ago

TLE from 11 hours ago
0 FR 1
1 01814U 65101A   25258.25339554  .00001007  00000-0  16688-3 0  9995
2 01814  75.8635 105.2622 0004601  69.3621 290.8053 14.70977099 15664
Epoch: 2025-09-15T06:04Z
TLE epoch observation values (Epoch: 2025-09-15T06:04:53.374Z)
Latitude
-0.0001°
Longitude
19.57908°
Altitude
659.555 km
Speed
7.528 km/s
True Right ascension
07h 01m 02s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
09:51:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
658.622 km
Perigee altitude
652.15 km
Semi-major axis
7,033.523 km
Eccentricity
0.00046
Inclination
75.8635°
RAAN
105.2622°
Arg. of periapsis
69.3621°
True anomaly
290.756°
Mean anomaly
290.8053°
Eccentric anomaly
290.78065°
Mean motion
3.67946 °/min
Orbital period
97.84 mins
BSTAR
0.00016688
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