OBJECT K, 61236 (Decayed)
Orbit data source: Space-Track
OBJECT K, 61236 was a satellite owned by Changzheng H. (CN) in LEO that was launched on Tue, 24 Sep 2024 UTC launched from the Yellow Sea Launch Area, China (YSLA). 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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61236 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 5 months ago
TLE from 5 months ago
0 OBJECT K
1 61236U 24173K 25248.36256531 .10875761 25328-5 76751-3 0 9996
2 61236 97.3746 338.0203 0013575 268.4411 91.5333 16.39957900 53698Epoch: 2025-09-05T08:42Z
TLE epoch observation values (Epoch: 2025-09-05T08:42:05.642Z)
Latitude
-0.00009°
Longitude
-137.21503°
Altitude
169.416 km
Speed
7.804 km/s
True Right ascension
22h 32m 04s
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
09:00:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
171.6 km
Perigee altitude
153.842 km
Semi-major axis
6,540.858 km
Eccentricity
0.00136
Inclination
97.3746°
RAAN
338.0203°
Arg. of periapsis
268.4411°
True anomaly
91.6888°
Mean anomaly
91.5333°
Eccentric anomaly
91.61105°
Mean motion
4.1029 °/min
Orbital period
87.74 mins
BSTAR
0.00076751
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Other satellites on launch #173 in the year 2024 (2024-09-24 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 K 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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