OBJECT A, 61227
Orbit data source: Space-Track
You're viewing an Uncataloged Satellite
Recently launched and/or uncataloged satellites may have evolving metadata. Metadata may include but not limited to: Owner, Maufacturer, Bus, Motor, and Mission.
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)
OBJECT A details
Identifier | |
Orbit | SSO |
Last TLE update | 9 hours ago |
Origin | |
Manufacturer | Taizhou Xingkong |
Mission | Operational spacecraft |
Bus & Motor | JTX, Unknown motor |
Mass | ~50 kg wet, ~50 kg dry |
Launch date (UTC) | |
Launch vehicle | |
Launch site | |
Object type | Unknown |
Shape & HBR | Unknown |
Radar Cross Section | Medium (>0.1 m² and <1 m²) |
Expand to show TLE details & history
TLE from 9 hours ago
0 OBJECT A
1 61227U 24173A 24356.13238487 .00003982 00000-0 14096-3 0 9996
2 61227 97.3982 68.2790 0008651 345.6932 14.4062 15.29694682 13421
Epoch: 2024-12-21T03:10Z
Definitive object data (Epoch: 2024-12-21T03:10:38.052Z)
Latitude | -0.00005° |
Longitude | -69.56747° |
Altitude | 474.083 km |
Speed | 7.632 km/s |
True Right ascension | 04h 33m 06s |
True Declination | 0° 00' 00" |
Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
Latitude | -14.57857° |
Longitude | -67.25495° |
Altitude | 476.905 km |
Speed | 7.63 km/s |
Apparent Right ascension | 02h 35m 28s |
Apparent Declination | -32° 29' 50" |
Sunlit | Object is in full shadow |
Visualization observer readout
Local Sidereal Time | 11:33:48 |
Azimuth | 266.933° W |
Elevation | -53.018° |
Doppler factor | 1 |
Orbital elements
Apogee altitude | 479.604 km |
Perigee altitude | 467.749 km |
Semi-major axis | 6,851.814 km |
Eccentricity | 0.0008651 |
Inclination | 97.3982° |
RAAN | 68.279° |
Arg. of periapsis | 345.6932° |
True anomaly | 14.43089° |
Mean anomaly | 14.4062° |
Eccentric anomaly | 14.41854° |
Mean motion | 3.82679 °/min |
BSTAR | 0.00014096 |
Orbital period | 94.07 mins |
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Other satellites on launch #173 in the year 2024 (2024-09-24 UTC)
OBJECT A, 61227 |
OBJECT B, 61228 |
OBJECT C, 61229 |
OBJECT D, 61230 |
OBJECT E, 61231 |
OBJECT F, 61232 |
OBJECT G, 61233 |
OBJECT H, 61234 |
OBJECT J, 61235 (Decayed) |
OBJECT K, 61236 |
OBJECT L, 61237 |
OBJECT A Visibility forecast
Observer location: undefined°, undefined
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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6 mins | 2024-12-21 17:51:59.865Z | 14.152° NNE | 2024-12-21 17:54:59.865Z | 121.519° SE | 44.725° | 2024-12-21 17:57:59.865Z | 189.93° SSW |
4 mins | 2024-12-22 04:26:59.865Z | 115.044° SE | 2024-12-22 04:28:59.865Z | 65.674° ENE | 23.274° | 2024-12-22 04:30:59.865Z | 22.141° NNE |
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