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.
Focus sentinelFocus sentinel
Embed this page
Focus sentinelFocus sentinel
2514 intel report (Beta)
Focus sentinelFocus sentinel
Create New Watchlist
Focus sentinelFocus sentinel
Edit Public Description
Identifier
Orbit
Country
Unknown / 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: 12 hours ago
TLE from 12 hours ago
0 INTELSAT 2-F1
1 02514U 66096A 25288.36279229 -.00000555 00000-0 00000-0 0 9990
2 02514 17.2087 102.1662 6377152 95.7714 335.1327 2.00471077 89909Epoch: 2025-10-15T08:42Z
TLE epoch observation values (Epoch: 2025-10-15T08:42:25.253Z)
Latitude
-0.00011°
Longitude
-52.50051°
Altitude
10,415.238 km
Speed
5.698 km/s
True Right ascension
06h 48m 58s
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
15:07:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
37,138.719 km
Perigee altitude
3,248.381 km
Semi-major axis
26,571.687 km
Eccentricity
0.63772
Inclination
17.2087°
RAAN
102.1662°
Arg. of periapsis
95.7714°
True anomaly
264.58476°
Mean anomaly
335.1327°
Eccentric anomaly
305.31955°
Mean motion
0.50109 °/min
Orbital period
718.44 mins
BSTAR
0
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Other satellites on launch #96 in the year 1966 (1966-10-26 UTC)
Did you know?
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
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. |
|---|---|---|---|---|---|---|---|
| 52 mins | 2025-10-15 21:33:07.532Z | 244.185° WSW | 2025-10-15 21:47:07.532Z | 183.45° SSW | 26.742° | 2025-10-15 22:25:07.532Z | 129.117° SE |
| 300 mins | 2025-10-16 03:28:07.532Z | 133.196° SE | 2025-10-16 07:04:07.532Z | 143.8° SSE | 18.232° | 2025-10-16 08:28:07.532Z | 123.431° SE |
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 |
|---|
CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
Authenticating...
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 ascending order |
|---|