CZ-6A DEB, 61477
Orbit data source: Space-Track
CZ-6A DEB, 61477 is space debris in LEO originally from a launch on Tue, 06 Aug 2024 UTC launched from the Taiyaun Space Center, China (TSC). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
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61477 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SAST
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 CZ-6A DEB
1 61477U 24140AAK 25261.08537720 .00005555 00000-0 11045-2 0 9997
2 61477 89.0421 304.6891 0105198 114.5391 246.6830 14.58492385 55132Epoch: 2025-09-18T02:02Z
TLE epoch observation values (Epoch: 2025-09-18T02:02:56.59Z)
Latitude
-0.00004°
Longitude
-83.29873°
Altitude
731.283 km
Speed
7.473 km/s
True Right ascension
20h 18m 45s
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
12:58:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
769.349 km
Perigee altitude
620.534 km
Semi-major axis
7,073.079 km
Eccentricity
0.01052
Inclination
89.0421°
RAAN
304.6891°
Arg. of periapsis
114.5391°
True anomaly
245.58177°
Mean anomaly
246.683°
Eccentric anomaly
246.13181°
Mean motion
3.64864 °/min
Orbital period
98.67 mins
BSTAR
0.0011045
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Other satellites on launch #140 in the year 2024 (2024-08-06 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.CZ-6A DEB 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-09-19 02:52:16.868Z | 147.866° SSE | 2025-09-19 02:56:16.868Z | 72.339° E | 31.919° | 2025-09-19 02:59:16.868Z | 20.344° NNE |
| 4 mins | 2025-09-19 04:33:16.868Z | 254.308° W | 2025-09-19 04:35:16.868Z | 286.326° WNW | 16.981° | 2025-09-19 04:37:16.868Z | 314.977° NW |
| 7 mins | 2025-09-19 14:51:16.868Z | 19.975° NNE | 2025-09-19 14:54:16.868Z | 82.585° E | 35.267° | 2025-09-19 14:58:16.868Z | 159.478° S |
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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