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MORELOS 1, 15824

Orbit data source: Space-Track

MORELOS 1, 15824 is a payload satellite owned by SCT (MX) in GEO that was launched on Mon, 17 Jun 1985 UTC via an SPACE SHUTTLE 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
15824, 1985-048B
Orbit
GEO
Country
Flag of MXMX / MEX
Related business
Manufacturer
Hughes
Mission
Spacecraft
Bus & Motor
HS-376, TE-M-700-17
Mass
1,156 kg wet, 464 kg dry
Launch date (UTC)
1985-06-17 (41 years ago)
Launch vehicle
SPACE SHUTTLE
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)

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Last TLE update: 1 day ago

TLE from 1 day ago
0 MORELOS 1
1 15824U 85048B   26093.42830169 -.00000094  00000-0  00000-0 0  9992
2 15824  13.9966 343.5195 0002158 130.0987  56.5124  0.99472678116508
Epoch: 2026-04-03T10:16Z
TLE epoch observation values (Epoch: 2026-04-03T10:16:45.266Z)
Latitude
-1.61262°
Longitude
-175.97032°
Altitude
36,006.863 km
Speed
3.067 km/s
True Right ascension
11h 19m 55s
True Declination
-1° 36' 40"
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
02:37:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,022.234 km
Perigee altitude
36,003.938 km
Semi-major axis
42,391.223 km
Eccentricity
0.00022
Inclination
13.9966°
RAAN
343.5195°
Arg. of periapsis
130.0987°
True anomaly
56.53303°
Mean anomaly
56.5124°
Eccentric anomaly
56.52271°
Mean motion
0.24867 °/min
Orbital period
1,447.68 mins
BSTAR
0
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