Showing default

MORELOS 3, 40946

Orbit data source: Space-Track

MORELOS 3, 40946 is a payload satellite owned by AEMX (MX) in GEO that was launched on Fri, 02 Oct 2015 UTC via an ATLAS V 421 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
40946, 2015-056A
Orbit
GEO
Country
Flag of MXMX / MEX
Related business
Manufacturer
Boeing/ES
Mission
Operational Civil Communications
Bus & Motor
BSS-702HP, R-4D
Mass
~5,400 kg wet, ~2,800 kg dry
Launch date (UTC)
2015-10-02 (11 years ago)
Launch vehicle
ATLAS V 421
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan + 1 Dish, 20.5 m
Radar Cross Section
62.043 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 6 days ago

TLE from 6 days ago
0 MORELOS 3
1 40946U 15056A   26155.23725381 -.00000032  00000-0  00000-0 0  9996
2 40946   3.1768  14.7367 0001804 349.4653 220.7886  1.00270788 39159
Epoch: 2026-06-04T05:41Z
TLE epoch observation values (Epoch: 2026-06-04T05:41:38.729Z)
Latitude
-1.61968°
Longitude
-113.15882°
Altitude
35,792.347 km
Speed
3.074 km/s
True Right ascension
14h 59m 44s
True Declination
-1° 37' 05"
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
06:11:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,795.547 km
Perigee altitude
35,780.333 km
Semi-major axis
42,166.077 km
Eccentricity
0.00018
Inclination
3.1768°
RAAN
14.7367°
Arg. of periapsis
349.4653°
True anomaly
220.7751°
Mean anomaly
220.7886°
Eccentric anomaly
220.78185°
Mean motion
0.25067 °/min
Orbital period
1,436.16 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 #56 in the year 2015 (2015-10-02 UTC)

Documentation

Showing up to 5 results
|