QAEM 100 DEB, 61181 (Decayed)
Orbit data source: Space-Track
QAEM 100 DEB, 61181 was space debris in LEO originally from a launch on Sat, 14 Sep 2024 UTC launched from the Sharud Missile Test Site (SMTS). 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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61181 intel report (Beta)
QAEM 100 DEB details
Identifier | |
Orbit | Decayed |
Last TLE update | 2 weeks ago |
Origin | |
Manufacturer | IRGC |
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 2 weeks ago
0 QAEM 100 DEB
1 61181U 24165C 24341.31806047 .07126369 11315+0 15088-1 0 9995
2 61181 64.0774 59.0800 0018345 357.9111 2.1970 16.03767282 12416
Epoch: 2024-12-06T07:38Z
Definitive object data (Epoch: 2024-12-06T07:38:00.424Z)
Latitude | -0° |
Longitude | -131.008° |
Altitude | 253.864 km |
Speed | 7.762 km/s |
True Right ascension | 03h 56m 19s |
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 | 274.769 km |
Perigee altitude | 250.404 km |
Semi-major axis | 6,640.723 km |
Eccentricity | 0.0018345 |
Inclination | 64.0774° |
RAAN | 59.08° |
Arg. of periapsis | 357.9111° |
True anomaly | 2.20508° |
Mean anomaly | 2.197° |
Eccentric anomaly | 2.20104° |
Mean motion | 4.0107 °/min |
BSTAR | 0.015088 |
Orbital period | 89.76 mins |
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Other satellites on launch #165 in the year 2024 (2024-09-14 UTC)
QAEM 100 R/B, 61071 |
CHAMRAN-1, 61072 |
QAEM 100 DEB, 61181 (Decayed) |
QAEM 100 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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