OBJECT F, 61232 (Decayed)
Orbit data source: Space-Track
OBJECT F, 61232 was a Chinese satellite in LEO that was launched on Tue, 24 Sep 2024 UTC via a JIELONG-3 launch vehicle 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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61232 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
None
Manufacturer
Unknown
Mission
Decayed Commercial Technology
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box + 3 Pan, 0.2 m
Radar Cross Section
0.135 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 month ago
TLE from 1 month ago
0 OBJECT F
1 61232U 24173F 26218.72219575 .16039537 25458-5 22253-3 0 9998
2 61232 97.3225 319.8814 0015309 261.5838 98.3731 16.48093631105647Epoch: 2026-08-06T17:19Z
TLE epoch observation values (Epoch: 2026-08-06T17:19:57.712Z)
Latitude
-0.00001°
Longitude
104.63277°
Altitude
149.094 km
Speed
7.816 km/s
True Right ascension
21h 19m 31s
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
10:59:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
151.134 km
Perigee altitude
131.174 km
Semi-major axis
6,519.291 km
Eccentricity
0.00153
Inclination
97.3225°
RAAN
319.8814°
Arg. of periapsis
261.5838°
True anomaly
98.54661°
Mean anomaly
98.3731°
Eccentric anomaly
98.45986°
Mean motion
4.12328 °/min
Orbital period
87.31 mins
BSTAR
0.00022253
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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 F 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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