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)
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Edit Public Description
Identifier
Orbit
Country
Unknown / IRANRelated business
Islamic Revolutionary Guard Corps (IRGC) (IR)Manufacturer
IRGC
Mission
Decayed spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 9 months ago
TLE from 9 months 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 12416Epoch: 2024-12-06T07:38Z
TLE epoch observation values (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
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
21:58:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
274.769 km
Perigee altitude
250.404 km
Semi-major axis
6,640.723 km
Eccentricity
0.00183
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
Orbital period
89.76 mins
BSTAR
0.015088
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Other satellites on launch #165 in the year 2024 (2024-09-14 UTC)
QAEM 100 DEB Visibility
Observer location: undefined°, undefined°
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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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