ATLAS H R/B, 14691 (Decayed)
Orbit data source: Space-Track
ATLAS H R/B, 14691 was space debris in LEO originally from a launch on Sun, 05 Feb 1984 UTC launched from the Air Force Western Test Range (AFWTR). 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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14691 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Last TLE update
3 months ago
Origin
Manufacturer
NRL
Mission
Decayed spacecraft
Bus & Motor
MSD-PS, Unknown motor
Mass
~20 kg wet, ~20 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 0.9 m
Radar Cross Section
1.414 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & history
TLE from 3 months ago
0 ATLAS H R/B
1 14691U 84012B 25093.18377309 .04973033 37253-1 17937-1 0 9991
2 14691 63.2347 28.5572 0022429 174.3008 185.8399 15.92712714307595Epoch: 2025-04-03T04:24Z
TLE epoch observation values (Epoch: 2025-04-03T04:24:37.994Z)
Latitude
-0.00004°
Longitude
130.63861°
Altitude
311.544 km
Speed
7.713 km/s
True Right ascension
01h 54m 13s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
No trajectory is available.
Visualization observer readout
No trajectory is available.
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Other satellites on launch #12 in the year 1984 (1984-02-05 UTC)
ATLAS H R/B Visibility
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. |
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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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Authenticating...
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