LEASAT 2 PKM, 15244 (Decayed)
Orbit data source: Space-Track
LEASAT 2 PKM, 15244 was space debris in LEO originally from a launch on Thu, 30 Aug 1984 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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15244 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Last TLE update
7 months ago
Origin
Manufacturer
Thiokol/UT
Mission
Decayed spacecraft
Bus & Motor
MM3-PKM, Unknown motor
Mass
~200 kg wet, ~200 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Sphere + Cone, 1.3 m
Radar Cross Section
3.557 m², Large (>1 m²)
Expand to show TLE details & history
TLE from 7 months ago
0 LEASAT 2 PKM
1 15244U 84093E 24356.01712207 .17237538 -10275-4 49792-3 0 9990
2 15244 27.1177 224.6125 0125969 223.8207 248.7800 16.22582430904365Epoch: 2024-12-21T00:24Z
TLE epoch observation values (Epoch: 2024-12-21T00:24:39.346Z)
Latitude
25.26034°
Longitude
-117.99232°
Altitude
241.64 km
Speed
7.749 km/s
True Right ascension
22h 32m 59s
True Declination
25° 07' 03"
Sunlit
Visualization orbit readout
No trajectory is available.
Visualization observer readout
No trajectory is available.
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Other satellites on launch #93 in the year 1984 (1984-08-30 UTC)
LEASAT 2 PKM 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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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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Authenticating...
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