QAEM 100 R/B, 61071
Orbit data source: Space-Track
QAEM 100 R/B, 61071 is 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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61071 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
Operational spacecraft
Bus & Motor
Unknown
Mass
~200 kg wet, ~200 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 0.8 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 QAEM 100 R/B
1 61071U 24165A 25311.80209781 .00007499 00000-0 42596-3 0 9998
2 61071 64.0762 42.8341 0048657 318.4756 41.2667 15.12644181 63343Epoch: 2025-11-07T19:15Z
TLE epoch observation values (Epoch: 2025-11-07T19:15:01.250Z)
Latitude
-0.00007°
Longitude
66.83802°
Altitude
504.917 km
Speed
7.626 km/s
True Right ascension
02h 51m 20s
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
20:04:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
560.381 km
Perigee altitude
493.187 km
Semi-major axis
6,904.921 km
Eccentricity
0.00487
Inclination
64.0762°
RAAN
42.8341°
Arg. of periapsis
318.4756°
True anomaly
41.63614°
Mean anomaly
41.2667°
Eccentric anomaly
41.45125°
Mean motion
3.78273 °/min
Orbital period
95.17 mins
BSTAR
0.00042596
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Other satellites on launch #165 in the year 2024 (2024-09-14 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.QAEM 100 R/B Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-11-08 08:05:02.131Z | 211.002° SW | 2025-11-08 08:09:02.131Z | 36.402° NE | 42.774° | 2025-11-08 08:12:02.131Z | 33.284° NE |
| 6 mins | 2025-11-08 16:25:02.131Z | 345.466° N | 2025-11-08 16:28:02.131Z | 79.098° E | 36.268° | 2025-11-08 16:31:02.131Z | 127.959° SE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
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