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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
Last TLE update
11 hours ago
Origin
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

TLE from 11 hours ago
0 FR 1
1 01814U 65101A   25199.48682711  .00000637  00000-0  10693-3 0  9998
2 01814  75.8637 206.5492 0005419 223.6084 136.4669 14.70854996  7021
Epoch: 2025-07-18T11:41Z
TLE epoch observation values (Epoch: 2025-07-18T11:41:01.862Z)
Latitude
-0.00009°
Longitude
94.75383°
Altitude
663.859 km
Speed
7.524 km/s
True Right ascension
13h 46m 11s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
0.18838°
Longitude
93.98055°
Altitude
663.895 km
Speed
7.524 km/s
Apparent Right ascension
16h 22m 25s
Apparent Declination
-49° 10' 40"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
11:54:16
Azimuth
141.029° SSE
Elevation
-16.856°
Doppler factor
1
Orbital elements
Apogee altitude
659.587 km
Perigee altitude
651.964 km
Semi-major axis
7,033.912 km
Eccentricity
0.00054
Inclination
75.8637°
RAAN
206.5492°
Arg. of periapsis
223.6084°
True anomaly
136.50965°
Mean anomaly
136.4669°
Eccentric anomaly
136.48828°
Mean motion
3.67915 °/min
Orbital period
97.85 mins
BSTAR
0.00010693
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