ASC 1 R/B(PAM-D), 16007
Orbit data source: Space-Track
ASC 1 R/B(PAM-D), 16007 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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16007 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Last TLE update
1 day ago
Origin
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, 2.3 m
Radar Cross Section
2.972 m², Large (>1 m²)
Expand to show TLE details & history
TLE from 1 day ago
0 ASC 1 R/B(PAM-D)
1 16007U 85076G 25196.39975926 .00000060 00000-0 41682-3 0 9993
2 16007 27.0740 359.9944 7147216 319.7402 4.8978 2.37722627338472Epoch: 2025-07-15T09:35Z
TLE epoch observation values (Epoch: 2025-07-15T09:35:39.2Z)
Latitude
0°
Longitude
-77.41388°
Altitude
1,117.186 km
Speed
9.463 km/s
True Right ascension
23h 59m 58s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
13.68355°
Longitude
73.75773°
Altitude
33,245.229 km
Speed
1.82 km/s
Apparent Right ascension
10h 19m 03s
Apparent Declination
7° 04' 06"
Sunlit
Visualization observer readout
Local Sidereal Time
00:17:21
Azimuth
37.074° NE
Elevation
-35.665°
Doppler factor
1
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Other satellites on launch #76 in the year 1985 (1985-08-27 UTC)
ASC 1 R/B(PAM-D) Visibility forecast
Observer location: undefined°, undefined°
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. |
|---|---|---|---|---|---|---|---|
| 546 mins | 2025-07-16 16:04:33.984Z | 244.024° WSW | 2025-07-16 16:46:33.984Z | 165.031° S | 43.327° | 2025-07-17 01:10:33.984Z | 178.091° S |
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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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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