INTELSAT 2-F1, 2514
Orbit data source: Space-Track
INTELSAT 2-F1, 2514 is a payload satellite owned by INTELSAT (US) in HEO that was launched on Wed, 26 Oct 1966 UTC via a THOR DELTA E1 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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2514 intel report (Beta)
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Identifier
Orbit
Country
US / ITSORelated business
Manufacturer
Hughes
Mission
Non-operational spacecraft
Bus & Motor
HS-303, SVM-1
Mass
162 kg wet, 64 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 INTELSAT 2-F1
1 02514U 66096A 26202.04586272 -.00000346 00000-0 00000-0 0 9999
2 02514 18.1399 48.8804 6390232 193.1354 135.5318 2.00327670 95498Epoch: 2026-07-21T01:06Z
TLE epoch observation values (Epoch: 2026-07-21T01:06:02.539Z)
Latitude
-0.00002°
Longitude
93.57309°
Altitude
35,237.605 km
Speed
2.04 km/s
True Right ascension
03h 15m 37s
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
17:48:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
37,194.19 km
Perigee altitude
3,218.188 km
Semi-major axis
26,584.326 km
Eccentricity
0.63902
Inclination
18.1399°
RAAN
48.8804°
Arg. of periapsis
193.1354°
True anomaly
166.87871°
Mean anomaly
135.5318°
Eccentric anomaly
152.4604°
Mean motion
0.50073 °/min
Orbital period
718.95 mins
BSTAR
0
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Other satellites on launch #96 in the year 1966 (1966-10-26 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.INTELSAT 2-F1 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. |
|---|---|---|---|---|---|---|---|
| 646 mins | 2026-07-22 09:20:30.965Z | 177.41° S | 2026-07-22 19:05:30.965Z | 181.667° SSW | 40.742° | 2026-07-22 20:06:30.965Z | 110.838° ESE |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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