Showing default

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.

Loading next visibility...
Identifier
2514, 1966-096A
Orbit
HEO
Last TLE update
1 day ago
Origin
Manufacturer
Hughes
Mission
Non-operational Civil Communications
Bus & Motor
HS-303, SVM-1
Mass
162 kg wet, 64 kg dry
Launch date (UTC)
1966-10-26 (59 years ago)
Launch vehicle
THOR DELTA E1
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 0.7 m
Radar Cross Section
2.199 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 1 day ago
0 INTELSAT 2-F1
1  2514U 66096A   25199.60037761 -.00000356  00000-0  00000+0 0  9999
2  2514  17.1596 119.3688 6355248  64.3570 346.6375  2.00528671306966
Epoch: 2025-07-18T14:24Z
TLE epoch observation values (Epoch: 2025-07-18T14:24:32.625Z)
Latitude
0.00007°
Longitude
-33.46703°
Altitude
6,055.671 km
Speed
7.008 km/s
True Right ascension
07h 57m 16s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
17.16994°
Longitude
51.4575°
Altitude
3,567.589 km
Speed
8.072 km/s
Apparent Right ascension
14h 19m 52s
Apparent Declination
-4° 42' 52"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
03:44:31
Azimuth
34.005° NE
Elevation
-49.958°
Doppler factor
1
Orbital elements
Apogee altitude
37,072.165 km
Perigee altitude
3,304.723 km
Semi-major axis
26,566.581 km
Eccentricity
0.63552
Inclination
17.1596°
RAAN
119.3688°
Arg. of periapsis
64.357°
True anomaly
295.10071°
Mean anomaly
346.6375°
Eccentric anomaly
326.58489°
Mean motion
0.50123 °/min
Orbital period
718.23 mins
BSTAR
0
Loading maneuver chart data...
Loading SW <> Apogee altitude chart data...
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)
|