OBJECT D, 62266 (Decayed)
Orbit data source: Space-Track
OBJECT D, 62266 was an Iranian satellite in LEO that was launched on Fri, 06 Dec 2024 UTC via an SIMORGH launch vehicle from the Semnan, Iran (SEM). Unknown objects in Earth's orbit typically refer to objects detected orbiting the Earth but have not yet been identified or cataloged. These objects could be anything from previously untracked satellites, spent rocket stages, debris from satellite collisions, or even natural meteoroids temporarily captured by Earth's gravity. This object's orbit decayed before it could be identified.
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62266 intel report (Beta)
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Identifier
Orbit
Country
Unknown / IRANRelated business
None
Manufacturer
Unknown
Mission
Decayed Defense Technology
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 OBJECT D
1 62266U 24236D 25039.05010051 .08588739 11096-4 41198-3 0 9995
2 62266 58.5319 101.9830 0010822 292.2957 67.7013 16.42071242 9996Epoch: 2025-02-08T01:12Z
TLE epoch observation values (Epoch: 2025-02-08T01:12:08.684Z)
Latitude
-0.00002°
Longitude
-54.45675°
Altitude
159.148 km
Speed
7.813 km/s
True Right ascension
06h 47m 55s
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
20:11:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
166.763 km
Perigee altitude
152.613 km
Semi-major axis
6,537.825 km
Eccentricity
0.00108
Inclination
58.5319°
RAAN
101.983°
Arg. of periapsis
292.2957°
True anomaly
67.8161°
Mean anomaly
67.7013°
Eccentric anomaly
67.75869°
Mean motion
4.10576 °/min
Orbital period
87.68 mins
BSTAR
0.00041198
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Other satellites on launch #236 in the year 2024 (2024-12-06 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.OBJECT D 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
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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