OPTUS A2 R/B(PAM-D), 16294

Orbit data source: Space-Track

OPTUS A2 R/B(PAM-D), 16294 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
16294, 1985-109G
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
Unknown
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 OPTUS A2 R/B(PAM-D)
1 16294U 85109G   26080.84422681  .00000241  00000-0  12200-2 0  9990
2 16294  25.9262 191.0098 7117535 173.8095 205.6499  2.39087742300178
Epoch: 2026-03-21T20:15Z
TLE epoch observation values (Epoch: 2026-03-21T20:15:41.196Z)
Latitude
-0°
Longitude
67.70637°
Altitude
33,497.676 km
Speed
1.766 km/s
True Right ascension
12h 43m 56s
True Declination
0° 00' 00"
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
12:11:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
34,067.87 km
Perigee altitude
432.668 km
Semi-major axis
23,628.406 km
Eccentricity
0.71175
Inclination
25.9262°
RAAN
191.0098°
Arg. of periapsis
173.8095°
True anomaly
186.20821°
Mean anomaly
205.6499°
Eccentric anomaly
195.05638°
Mean motion
0.59757 °/min
Orbital period
602.44 mins
BSTAR
0.00122
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