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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1814 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
FRRelated business
Manufacturer
Nord
Mission
Spacecraft
Bus & Motor
FR, Unknown motor
Mass
62 kg wet, 62 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 FR 1
1 1814U 65101A 25319.52937347 .00001799 00000-0 29452-3 0 9998
2 1814 75.8680 359.6130 0006126 277.3720 82.6765 14.71198018 24673Epoch: 2025-11-15T12:42Z
TLE epoch observation values (Epoch: 2025-11-15T12:42:17.867Z)
Latitude
-0.00009°
Longitude
114.18132°
Altitude
659.453 km
Speed
7.528 km/s
True Right ascension
23h 58m 27s
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
03:34:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
658.989 km
Perigee altitude
650.373 km
Semi-major axis
7,032.818 km
Eccentricity
0.00061
Inclination
75.868°
RAAN
359.613°
Arg. of periapsis
277.372°
True anomaly
82.74613°
Mean anomaly
82.6765°
Eccentric anomaly
82.71132°
Mean motion
3.68001 °/min
Orbital period
97.83 mins
BSTAR
0.00029452
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Other satellites on launch #101 in the year 1965 (1965-12-06 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.FR 1 Visibility forecast
Loading observer location...
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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-11-16 13:44:55.124Z | 2.52° NNE | 2025-11-16 13:47:55.124Z | 53.314° ENE | 33.377° | 2025-11-16 13:51:55.124Z | 136.507° SSE |
| 4 mins | 2025-11-16 15:25:55.124Z | 288.548° WNW | 2025-11-16 15:27:55.124Z | 257.283° W | 16.338° | 2025-11-16 15:29:55.124Z | 229.755° WSW |
| 7 mins | 2025-11-17 04:00:55.124Z | 210.042° SW | 2025-11-17 04:03:55.124Z | 285.546° WNW | 42.194° | 2025-11-17 04:07:55.124Z | 9.008° NNE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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