Showing default

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.

Loading next visibility...
Identifier
56174, 2023-052A
Orbit
GEO
Country
Flag of UnknownUnknown / ITSO
Related business
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 (3 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
Last TLE update: 9 hours ago

TLE from 9 hours ago
0 INTELSAT 40E
1 56174U 23052A   26008.22200980 -.00000170  00000-0  00000-0 0  9993
2 56174   0.0162  70.6569 0001447 183.3743 202.6547  1.00271805 10227
Epoch: 2026-01-08T05:19Z
TLE epoch observation values (Epoch: 2026-01-08T05:19:41.646Z)
Latitude
0.02044°
Longitude
-91.00319°
Altitude
35,791.724 km
Speed
3.074 km/s
True Right ascension
06h 26m 47s
True Declination
0° 01' 13"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
14:19:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,793.761 km
Perigee altitude
35,781.558 km
Semi-major axis
42,165.797 km
Eccentricity
0.00014
Inclination
0.0162°
RAAN
70.6569°
Arg. of periapsis
183.3743°
True anomaly
202.64831°
Mean anomaly
202.6547°
Eccentric anomaly
202.65151°
Mean motion
0.25067 °/min
Orbital period
1,436.15 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 #52 in the year 2023 (2023-04-07 UTC)

Documentation

Showing up to 5 results
|