Showing default

INTELSAT 1-F1, 1317

Orbit data source: Space-Track

INTELSAT 1-F1, 1317 is a payload satellite owned by INTELSAT (US) in GEO that was launched on Tue, 06 Apr 1965 UTC via a THOR DELTA D 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
1317, 1965-028A
Orbit
GEO
Last TLE update
1 day ago
Origin
Manufacturer
Hughes
Mission
Non-operational Civil Communications
Bus & Motor
HS-303A, STARFINDER
Mass
68 kg wet, 30 kg dry
Launch date (UTC)
1965-04-06 (60 years ago)
Launch vehicle
THOR DELTA D
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 0.72 m
Radar Cross Section
0.543 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 1 day ago
0 INTELSAT 1-F1
1 01317U 65028A   25181.13005997 -.00000285  00000-0  00000-0 0  9990
2 01317   6.2978  67.2790 0006390 128.1200  82.3684  1.00271716123641
Epoch: 2025-06-30T03:07Z
TLE epoch observation values (Epoch: 2025-06-30T03:07:17.181Z)
Latitude
-3.21865°
Longitude
-47.55863°
Altitude
35,783.059 km
Speed
3.075 km/s
True Right ascension
18h 30m 49s
True Declination
-3° 12' 55"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
-5.81292°
Longitude
35.15727°
Altitude
35,813.118 km
Speed
3.073 km/s
Apparent Right ascension
00h 25m 43s
Apparent Declination
-11° 53' 54"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
20:10:34
Azimuth
116.383° SE
Elevation
11.49°
Doppler factor
1
Orbital elements
Apogee altitude
35,814.61 km
Perigee altitude
35,760.722 km
Semi-major axis
42,165.803 km
Eccentricity
0.00064
Inclination
6.2978°
RAAN
67.279°
Arg. of periapsis
128.12°
True anomaly
Unknown
Mean anomaly
82.3684°
Eccentric anomaly
Unknown
Mean motion
0.25067 °/min
Orbital period
1,436.15 mins
BSTAR
0
Loading historical data...
1317 neighbors
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 #28 in the year 1965 (1965-04-06 UTC)

INTELSAT 1-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.
1440 mins2025-07-01 08:32:26.613Z116.397° SE2025-07-01 18:45:26.613Z107.07° ESE19.303°2025-07-02 08:32:26.613Z116.367° SE
|