TRANSIT 16 DEB, 33508 (Decayed)
Orbit data source: Space-Track
TRANSIT 16 DEB, 33508 was space debris in LEO originally from a launch on Thu, 18 May 1967 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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33508 intel report (Beta)
TRANSIT 16 DEB details
Identifier | |
Orbit | Decayed |
Last TLE update | 4 months ago |
Origin | |
Manufacturer | Unknown |
Mission | Decayed spacecraft |
Bus & Motor | Unknown |
Mass | Unknown |
Launch date (UTC) | |
Launch vehicle | Unknown |
Launch site | |
Object type | Payload Rocket body Debris |
Shape & HBR | Unknown |
Radar Cross Section | Small (<0.1 m²) |
Expand to show TLE details & history
TLE from 4 months ago
0 TRANSIT 16 DEB
1 33508U 67048G 24235.79972159 .15470437 00000-0 14014+0 0 9999
2 33508 89.5126 340.6395 0043991 313.0328 46.7257 15.60671670828488
Epoch: 2024-08-22T19:11Z
Definitive object data (Epoch: 2024-08-22T19:11:35.945Z)
Latitude | -0.00006° |
Longitude | 81.15737° |
Altitude | 368.637 km |
Speed | 7.7 km/s |
True Right ascension | 22h 42m 33s |
True Declination | 0° 00' 00" |
Sunlit | Object was in full shadow at TLE epoch |
Visualization observer readout
Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed. |
Visualization observer readout
Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed. |
Orbital elements
Apogee altitude | 412.207 km |
Perigee altitude | 352.725 km |
Semi-major axis | 6,760.603 km |
Eccentricity | 0.0043991 |
Inclination | 89.5126° |
RAAN | 340.6395° |
Arg. of periapsis | 313.0328° |
True anomaly | 47.09411° |
Mean anomaly | 46.7257° |
Eccentric anomaly | 46.90977° |
Mean motion | 3.9045 °/min |
BSTAR | 0.14014 |
Orbital period | 92.2 mins |
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Other satellites on launch #48 in the year 1967 (1967-05-18 UTC)
TRANSIT 16 DEB 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. |
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