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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Edit Public Description
Identifier
Orbit
Country
Unknown / ITSORelated business
Manufacturer
Hughes
Mission
Non-operational Civil Communications
Bus & Motor
HS-303, SVM-1
Mass
162 kg wet, 64 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl, 0.7 m
Radar Cross Section
2.199 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 22 hours ago
TLE from 22 hours ago
0 INTELSAT 2-F1
1 02514U 66096A 25242.48370684 -.00000489 00000-0 00000-0 0 9996
2 02514 17.1673 111.1450 6366857 79.4235 342.0194 2.00502765 88986Epoch: 2025-08-30T11:36Z
TLE epoch observation values (Epoch: 2025-08-30T11:36:32.27Z)
Latitude
-0.00024°
Longitude
-41.7758°
Altitude
7,720.847 km
Speed
6.445 km/s
True Right ascension
07h 25m 06s
True Declination
0° 00' 01"
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
01:32:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
37,106.769 km
Perigee altitude
3,274.717 km
Semi-major axis
26,568.88 km
Eccentricity
0.63669
Inclination
17.1673°
RAAN
111.145°
Arg. of periapsis
79.4235°
True anomaly
280.58539°
Mean anomaly
342.0194°
Eccentric anomaly
317.26344°
Mean motion
0.50117 °/min
Orbital period
718.32 mins
BSTAR
0
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Other satellites on launch #96 in the year 1966 (1966-10-26 UTC)
INTELSAT 2-F1 Visibility forecast
Observer location: undefined°, undefined°
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. |
|---|---|---|---|---|---|---|---|
| 66 mins | 2025-08-31 09:53:26.379Z | 146.96° SSE | 2025-08-31 09:53:26.379Z | 146.96° SSE | 16.524° | 2025-08-31 10:59:26.379Z | 132.271° SE |
| 70 mins | 2025-09-01 00:11:26.379Z | 241.93° WSW | 2025-09-01 00:25:26.379Z | 180.343° SSW | 30.265° | 2025-09-01 01:21:26.379Z | 122.448° SE |
| 265 mins | 2025-09-01 05:28:26.379Z | 132.243° SE | 2025-09-01 09:13:26.379Z | 147.987° SSE | 16.962° | 2025-09-01 09:53:26.379Z | 146.576° SSE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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Authenticating...
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