OBJECT A, 61227
Orbit data source: Space-Track
OBJECT A, 61227 is a Chinese satellite in SSO 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.
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61227 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
None
Manufacturer
Unknown
Mission
Operational Commercial Imaging
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box + 1 Pan, 2.5 m
Radar Cross Section
5.339 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 OBJECT A
1 61227U 24173A 26190.14788722 .00162684 00000-0 95879-3 0 9990
2 61227 97.3364 279.2583 0006340 198.4686 161.6352 15.77697033100523Epoch: 2026-07-09T03:32Z
TLE epoch observation values (Epoch: 2026-07-09T03:32:57.455Z)
Latitude
0.00003°
Longitude
-61.07508°
Altitude
344.179 km
Speed
7.7 km/s
True Right ascension
18h 37m 01s
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
06:40:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
338.109 km
Perigee altitude
329.598 km
Semi-major axis
6,711.991 km
Eccentricity
0.00063
Inclination
97.3364°
RAAN
279.2583°
Arg. of periapsis
198.4686°
True anomaly
161.65807°
Mean anomaly
161.6352°
Eccentric anomaly
161.64664°
Mean motion
3.94699 °/min
Orbital period
91.21 mins
BSTAR
0.00095879
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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 A 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. |
|---|---|---|---|---|---|---|---|
| OBJECT A is likely not visible in the next few days. |
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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