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
Civil Science
Bus & Motor
FR, Unknown motor
Mass
62 kg wet, 62 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
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 & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 FR 1
1 01814U 65101A 25259.61367508 .00000779 00000-0 12969-3 0 9999
2 01814 75.8633 102.9169 0004616 65.6188 294.5474 14.70977503 15865Epoch: 2025-09-16T14:43Z
TLE epoch observation values (Epoch: 2025-09-16T14:43:41.526Z)
Latitude
-0.00014°
Longitude
-113.80762°
Altitude
659.355 km
Speed
7.529 km/s
True Right ascension
06h 51m 40s
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
21:34:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
658.631 km
Perigee altitude
652.138 km
Semi-major axis
7,033.522 km
Eccentricity
0.00046
Inclination
75.8633°
RAAN
102.9169°
Arg. of periapsis
65.6188°
True anomaly
294.49927°
Mean anomaly
294.5474°
Eccentric anomaly
294.52334°
Mean motion
3.67946 °/min
Orbital period
97.84 mins
BSTAR
0.00012969
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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
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-09-17 13:42:55.597Z | 135.053° SSE | 2025-09-17 13:45:55.597Z | 87.824° E | 18.817° | 2025-09-17 13:47:55.597Z | 57.956° ENE |
| 6 mins | 2025-09-17 15:21:55.597Z | 235.963° WSW | 2025-09-17 15:24:55.597Z | 299.842° NW | 30.2° | 2025-09-17 15:27:55.597Z | 352.827° N |
| 5 mins | 2025-09-17 23:56:55.597Z | 31.56° NE | 2025-09-17 23:58:55.597Z | 64.172° ENE | 18.764° | 2025-09-18 00:01:55.597Z | 107.4° ESE |
| 6 mins | 2025-09-18 01:35:55.597Z | 315.556° NNW | 2025-09-18 01:38:55.597Z | 244.788° WSW | 31.465° | 2025-09-18 01:41:55.597Z | 196.242° SSW |
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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