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)
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Edit Public Description
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: 6 hours ago
TLE from 6 hours ago
0 OBJECT A
1 61227U 24173A 25302.48407815 .00045154 00000-0 11330-2 0 9993
2 61227 97.3646 19.5902 0005625 26.9538 333.1999 15.39868870 61258Epoch: 2025-10-29T11:37Z
TLE epoch observation values (Epoch: 2025-10-29T11:37:04.352Z)
Latitude
-0.00002°
Longitude
167.26551°
Altitude
446.188 km
Speed
7.646 km/s
True Right ascension
01h 18m 21s
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
13:14:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
447.271 km
Perigee altitude
439.597 km
Semi-major axis
6,821.571 km
Eccentricity
0.00056
Inclination
97.3646°
RAAN
19.5902°
Arg. of periapsis
26.9538°
True anomaly
333.17082°
Mean anomaly
333.1999°
Eccentric anomaly
333.18536°
Mean motion
3.85227 °/min
Orbital period
93.45 mins
BSTAR
0.001133
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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 forecast
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-29 18:25:05.144Z | 356.418° N | 2025-10-29 18:27:05.144Z | 309.106° NW | 36.602° | 2025-10-29 18:30:05.144Z | 211.523° SW |
| 5 mins | 2025-10-30 04:55:05.144Z | 133.095° SE | 2025-10-30 04:57:05.144Z | 75.286° E | 31.178° | 2025-10-30 05:00:05.144Z | 5.783° NNE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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