CZ-6A DEB, 61827
Orbit data source: Space-Track
CZ-6A DEB, 61827 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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61827 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 shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 CZ-6A DEB
1 61827U 24140ACT 25326.35744774 .00003516 00000-0 19114-2 0 9997
2 61827 88.8561 291.4459 0104042 172.2083 188.0749 14.09359727 61494Epoch: 2025-11-22T08:34Z
TLE epoch observation values (Epoch: 2025-11-22T08:34:43.484Z)
Latitude
0°
Longitude
101.17744°
Altitude
939.209 km
Speed
7.344 km/s
True Right ascension
19h 25m 47s
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
22:44:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
933.822 km
Perigee altitude
783.239 km
Semi-major axis
7,236.667 km
Eccentricity
0.0104
Inclination
88.8561°
RAAN
291.4459°
Arg. of periapsis
172.2083°
True anomaly
187.90956°
Mean anomaly
188.0749°
Eccentric anomaly
187.99202°
Mean motion
3.52562 °/min
Orbital period
102.11 mins
BSTAR
0.0019114
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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 | 2025-11-23 09:01:56.573Z | 32.834° NE | 2025-11-23 09:05:56.573Z | 85.095° E | 20.366° | 2025-11-23 09:08:56.573Z | 124.715° SE |
| 7 mins | 2025-11-23 10:44:56.573Z | 334.717° NNW | 2025-11-23 10:47:56.573Z | 279.192° WNW | 32.779° | 2025-11-23 10:51:56.573Z | 213.927° SW |
| 10 mins | 2025-11-23 22:10:56.573Z | 176.62° S | 2025-11-23 22:15:56.573Z | 6.84° NNE | 44.299° | 2025-11-23 22:20:56.573Z | 359.819° N |
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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