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INTELSAT 40E, 56174

Orbit data source: Space-Track

INTELSAT 40E, 56174 is a payload satellite owned by Intelsat SA (US) (US) in GEO that was launched on Fri, 07 Apr 2023 UTC via an FALCON 9 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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Identifier
56174, 2023-052A
Orbit
GEO
Last TLE update
11 hours ago
Origin
Manufacturer
Maxar Space Sol
Mission
Operational Commercial Communications
Bus & Motor
LS-1300, R-4D
Mass
6,161 kg wet, ~3,000 kg dry
Launch date (UTC)
2023-04-07 (2 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 13.0 m
Radar Cross Section
98.099 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 11 hours ago
0 INTELSAT 40E
1 56174U 23052A   25199.53871811 -.00000168  00000-0  00000-0 0  9991
2 56174   0.0137  96.2324 0002133  49.4816 253.8018  1.00271505  8470
Epoch: 2025-07-18T12:55Z
TLE epoch observation values (Epoch: 2025-07-18T12:55:45.244Z)
Latitude
-0.01336°
Longitude
-91.03002°
Altitude
35,788.647 km
Speed
3.075 km/s
True Right ascension
02h 37m 59s
True Declination
0° 00' 48"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
0.02072°
Longitude
67.07405°
Altitude
35,780.648 km
Speed
3.075 km/s
Apparent Right ascension
13h 17m 43s
Apparent Declination
-6° 11' 04"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
12:13:52
Azimuth
158.552° S
Elevation
41.605°
Doppler factor
1
Orbital elements
Apogee altitude
35,796.738 km
Perigee altitude
35,778.75 km
Semi-major axis
42,165.881 km
Eccentricity
0.00021
Inclination
0.0137°
RAAN
96.2324°
Arg. of periapsis
49.4816°
True anomaly
253.77833°
Mean anomaly
253.8018°
Eccentric anomaly
253.79006°
Mean motion
0.25067 °/min
Orbital period
1,436.15 mins
BSTAR
0
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