QASED R/B, 51955 (Decayed)
Orbit data source: Space-Track
QASED R/B, 51955 was space debris in LEO originally from a launch on Tue, 08 Mar 2022 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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51955 intel report (Beta)
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Identifier
Orbit
Country
IR / IRANRelated business
Manufacturer
IRGC
Mission
Decayed spacecraft
Bus & Motor
QASED S3, Unknown motor
Mass
~100 kg wet, ~100 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 0.3 m
Radar Cross Section
0.153 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 QASED R/B
1 51955U 22024B 25114.31161047 .03834833 10894-4 70891-3 0 9997
2 51955 58.2542 118.6364 0003250 307.4572 52.6242 16.31660006175766Epoch: 2025-04-24T07:28Z
TLE epoch observation values (Epoch: 2025-04-24T07:28:43.144Z)
Latitude
-0.00004°
Longitude
153.87175°
Altitude
188.28 km
Speed
7.795 km/s
True Right ascension
07h 54m 32s
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
00:31:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
189.652 km
Perigee altitude
185.384 km
Semi-major axis
6,565.655 km
Eccentricity
0.00033
Inclination
58.2542°
RAAN
118.6364°
Arg. of periapsis
307.4572°
True anomaly
52.6538°
Mean anomaly
52.6242°
Eccentric anomaly
52.639°
Mean motion
4.07968 °/min
Orbital period
88.24 mins
BSTAR
0.00070891
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Other satellites on launch #24 in the year 2022 (2022-03-08 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.QASED R/B Visibility
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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. |
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| This satellite is decayed. |
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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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