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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
16 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, 26 m
Radar Cross Section
98.099 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 16 hours ago
0 INTELSAT 40E
1 56174U 23052A   25191.36297565 -.00000161  00000-0  00000-0 0  9995
2 56174   0.0168  67.5728 0002218  64.8050 195.8223  1.00271563  8396
Epoch: 2025-07-10T08:42Z
TLE epoch observation values (Epoch: 2025-07-10T08:42:41.096Z)
Latitude
-0.03774°
Longitude
-91.00522°
Altitude
35,795.168 km
Speed
3.074 km/s
True Right ascension
21h 52m 47s
True Declination
0° 02' 16"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
0.01562°
Longitude
151.69289°
Altitude
35,784.344 km
Speed
3.075 km/s
Apparent Right ascension
14h 10m 54s
Apparent Declination
-6° 11' 22"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
13:06:59
Azimuth
158.535° S
Elevation
41.596°
Doppler factor
1
Orbital elements
Apogee altitude
35,797.08 km
Perigee altitude
35,778.375 km
Semi-major axis
42,165.865 km
Eccentricity
0.00022
Inclination
0.0168°
RAAN
67.5728°
Arg. of periapsis
64.805°
True anomaly
Unknown
Mean anomaly
195.8223°
Eccentric anomaly
Unknown
Mean motion
0.25067 °/min
Orbital period
1,436.15 mins
BSTAR
0
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56174 neighbors
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Other satellites on launch #52 in the year 2023 (2023-04-07 UTC)

INTELSAT 40E 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 mins2025-07-11 00:50:41.859Z158.543° S2025-07-11 20:55:41.859Z158.554° S33.589°2025-07-12 00:50:41.859Z158.542° S
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