OPTUS A1 R/B(PAM-D), 15996

Orbit data source: Space-Track

OPTUS A1 R/B(PAM-D), 15996 is space debris in HEO originally from a launch on Tue, 27 Aug 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
15996, 1985-076E
Orbit
HEO
Last TLE update
19 hours ago
Origin
Manufacturer
Thiokol/TE
Mission
Spacecraft
Bus & Motor
STAR 48, Unknown motor
Mass
132 kg wet, 132 kg dry
Launch date (UTC)
1985-08-27 (40 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Sphere + Cone, 2.3 m
Radar Cross Section
2.972 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 19 hours ago
0 OPTUS A1 R/B(PAM-D)
1 15996U 85076E   25196.67316269  .00000157  00000-0  64085-3 0  9998
2 15996  26.3957 321.3469 7139103 107.8517 336.5041  2.38631441286892
Epoch: 2025-07-15T16:09Z
TLE epoch observation values (Epoch: 2025-07-15T16:09:21.256Z)
Latitude
0.00001°
Longitude
145.23171°
Altitude
8,475.363 km
Speed
6.068 km/s
True Right ascension
21h 25m 20s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
-11.50647°
Longitude
120.75581°
Altitude
17,056.09 km
Speed
4.143 km/s
Apparent Right ascension
18h 59m 11s
Apparent Declination
-22° 08' 38"
Sunlit
Object is in full shadow
Visualization observer readout
Local Sidereal Time
00:12:40
Azimuth
245.737° WSW
Elevation
-5.661°
Doppler factor
1
Orbital elements
Apogee altitude
34,170.395 km
Perigee altitude
390.314 km
Semi-major axis
23,658.491 km
Eccentricity
0.71391
Inclination
26.3957°
RAAN
321.3469°
Arg. of periapsis
107.8517°
True anomaly
Unknown
Mean anomaly
336.5041°
Eccentric anomaly
Unknown
Mean motion
0.59643 °/min
Orbital period
603.59 mins
BSTAR
0.00064085
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