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 week ago
TLE from 1 week ago
0 INTELSAT 2-F1
1 02514U 66096A 26149.71774270 -.00000369 00000-0 00000-0 0 9995
2 02514 17.9484 58.4852 6399129 175.3036 196.2703 2.00346290 94448Epoch: 2026-05-29T17:13Z
TLE epoch observation values (Epoch: 2026-05-29T17:13:32.969Z)
Latitude
0.00006°
Longitude
-87.17603°
Altitude
36,986.404 km
Speed
1.841 km/s
True Right ascension
03h 53m 49s
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
03:53:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
37,215.174 km
Perigee altitude
3,193.95 km
Semi-major axis
26,582.699 km
Eccentricity
0.63991
Inclination
17.9484°
RAAN
58.4852°
Arg. of periapsis
175.3036°
True anomaly
184.66734°
Mean anomaly
196.2703°
Eccentric anomaly
189.94087°
Mean motion
0.50078 °/min
Orbital period
718.88 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. |
|---|---|---|---|---|---|---|---|
| 243 mins | 2026-06-08 17:45:15.711Z | 164.077° S | 2026-06-08 20:38:15.711Z | 166.704° S | 39.515° | 2026-06-08 21:48:15.711Z | 103.733° ESE |
| 390 mins | 2026-06-09 11:15:15.711Z | 157.993° S | 2026-06-09 17:45:15.711Z | 164.775° S | 36.194° | 2026-06-09 17:45:15.711Z | 164.775° S |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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