CZ-6A DEB, 63392

Orbit data source: Space-Track

CZ-6A DEB, 63392 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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Iframe URL

https://www.satcat.com/sats-embedded/63392?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

63392, 2024-140ADP

Orbit

LEO

Country

CN / PRC

Related business

China National Space Administration (CN)

Manufacturer

SAST

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

2024-08-06 (2 years ago)

Launch vehicle

Unknown

Launch site

Taiyaun Space Center, China (TSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 0.1 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 15 hours ago

TLE from 15 hours ago

0 CZ-6A DEB
1 63392U 24140ADP 26171.24300627  .00000293  00000-0  12718-3 0  9991
2 63392  89.0332 276.7442 0037864 170.0708 190.1239 14.21191002 94383

Epoch: 2026-06-20T05:49Z

TLE epoch observation values (Epoch: 2026-06-20T05:49:55.741Z)

Latitude

-0.00011°

Longitude

-79.19849°

Altitude

851.227 km

Speed

7.413 km/s

True Right ascension

18h 26m 58s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

Latitude

Unknown

Longitude

Unknown

Altitude

Unknown

Speed

Unknown

Apparent Right ascension

Unknown

Apparent Declination

Unknown

Sunlit

N/A

Visualization observer readout

Local Sidereal Time

07:23:56

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

845.526 km

Perigee altitude

791.028 km

Semi-major axis

7,196.414 km

Eccentricity

0.00379

Inclination

89.0332°

RAAN

276.7442°

Arg. of periapsis

170.0708°

True anomaly

190.04799°

Mean anomaly

190.1239°

Eccentric anomaly

190.08591°

Mean motion

3.55524 °/min

Orbital period

101.26 mins

BSTAR

0.00012718

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Other satellites on launch #140 in the year 2024 (2024-08-06 UTC)

CZ-6A DEB, 60882

CZ-6A DEB, 61384 (Decayed)

CZ-6A DEB, 60744 (Decayed)

CZ-6A DEB, 60849

CZ-6A DEB, 60885

CZ-6A DEB, 61344 (Decayed)

CZ-6A DEB, 60711

CZ-6A DEB, 60799

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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.
10 mins	2026-06-21 07:17:09.865Z	169.63° S	2026-06-21 07:22:09.865Z	75.85° E	43.779°	2026-06-21 07:27:09.865Z	3.374° NNE
8 mins	2026-06-21 19:36:09.865Z	350.675° N	2026-06-21 19:40:09.865Z	255.449° W	41.455°	2026-06-21 19:44:09.865Z	196.313° SSW

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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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Check out CZ-6A DEB, 63392 on other resources

View CZ-6A DEB, 63392 on Heavens-Above

View CZ-6A DEB, 63392 on Keep Track

View CZ-6A DEB, 63392 on Celestrak

View CZ-6A DEB, 63392 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

CZ-6A DEB, 63392

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 15 hours ago

TLE from 15 hours ago

TLE epoch observation values (Epoch: 2026-06-20T05:49:55.741Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #140 in the year 2024 (2024-08-06 UTC)

CZ-6A DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out CZ-6A DEB, 63392 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 15 hours ago