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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16294 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Thiokol/TE
Mission
Spacecraft
Bus & Motor
STAR 48, Unknown motor
Mass
132 kg wet, 132 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Sphere + Cone, 1.1 m
Radar Cross Section
2.822 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 OPTUS A2 R/B(PAM-D)
1 16294U 85109G 25258.13647838 .00000775 00000-0 10844-2 0 9995
2 16294 25.9594 263.7110 7155567 51.7357 353.3391 2.38838266295685Epoch: 2025-09-15T03:16Z
TLE epoch observation values (Epoch: 2025-09-15T03:16:31.732Z)
Latitude
0.00001°
Longitude
-139.82612°
Altitude
1,604.259 km
Speed
9.111 km/s
True Right ascension
17h 34m 36s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
14:00:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
34,186.051 km
Perigee altitude
347.5 km
Semi-major axis
23,644.912 km
Eccentricity
0.71556
Inclination
25.9594°
RAAN
263.711°
Arg. of periapsis
51.7357°
True anomaly
308.8449°
Mean anomaly
353.3391°
Eccentric anomaly
337.94308°
Mean motion
0.59695 °/min
Orbital period
603.07 mins
BSTAR
0.0010844
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Other satellites on launch #109 in the year 1985 (1985-11-27 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.OPTUS A2 R/B(PAM-D) Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-09-17 05:46:55.210Z | 182.258° SSW | 2025-09-17 05:48:55.210Z | 148.37° SSE | 14.151° | 2025-09-17 05:51:55.210Z | 119.989° SE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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