MORELOS 2 R/B(PAM-D), 16293

Orbit data source: Space-Track

MORELOS 2 R/B(PAM-D), 16293 is space debris in HEO originally from a launch on Wed, 27 Nov 1985 UTC launched from the Air Force Eastern Test Range (AFETR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

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Identifier
16293, 1985-109F
Orbit
HEO
Country
Flag of USUS
Related business
Manufacturer
Thiokol/TE
Mission
Spacecraft
Bus & Motor
STAR 48, Unknown motor
Mass
132 kg wet, 132 kg dry
Launch date (UTC)
1985-11-27 (40 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Sphere + Cone, 1.1 m
Radar Cross Section
2.822 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 3 days ago

TLE from 3 days ago
0 MORELOS 2 R/B(PAM-D)
1 16293U 85109F   25256.92307295  .00000998  00000-0  17352-2 0  9997
2 16293  25.8163 287.2725 7160609 240.3011  31.3674  2.37473132274213
Epoch: 2025-09-13T22:09Z
TLE epoch observation values (Epoch: 2025-09-13T22:09:13.502Z)
Latitude
-0.00017°
Longitude
-38.19519°
Altitude
11,521.548 km
Speed
5.267 km/s
True Right ascension
19h 09m 02s
True Declination
0° 00' 01"
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
13:59:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
34,353.319 km
Perigee altitude
361.282 km
Semi-major axis
23,735.437 km
Eccentricity
0.71606
Inclination
25.8163°
RAAN
287.2725°
Arg. of periapsis
240.3011°
True anomaly
119.59573°
Mean anomaly
31.3674°
Eccentric anomaly
69.89452°
Mean motion
0.59354 °/min
Orbital period
606.53 mins
BSTAR
0.0017352
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