OBJECT B, 61228 (Decayed)
Orbit data source: Space-Track
OBJECT B, 61228 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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61228 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 4 months ago
TLE from 4 months ago
0 OBJECT B
1 61228U 24173B 25308.14047046 .18698425 25528-5 32238-3 0 9991
2 61228 97.3240 34.9924 0009730 265.1758 94.8434 16.47398128 62784Epoch: 2025-11-04T03:22Z
TLE epoch observation values (Epoch: 2025-11-04T03:22:16.647Z)
Latitude
-0.0001°
Longitude
-59.20871°
Altitude
150.002 km
Speed
7.816 km/s
True Right ascension
02h 19m 58s
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
23:32:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
149.336 km
Perigee altitude
136.646 km
Semi-major axis
6,521.128 km
Eccentricity
0.00097
Inclination
97.324°
RAAN
34.9924°
Arg. of periapsis
265.1758°
True anomaly
94.95449°
Mean anomaly
94.8434°
Eccentric anomaly
94.89895°
Mean motion
4.12154 °/min
Orbital period
87.35 mins
BSTAR
0.00032238
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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 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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