CZ-6A DEB, 63391

Orbit data source: Space-Track

CZ-6A DEB, 63391 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/63391?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

63391, 2024-140ADN

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

Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 17 hours ago

TLE from 17 hours ago

0 CZ-6A DEB
1 63391U 24140ADN 26118.19113962  .00000385  00000-0  18406-3 0  9991
2 63391  88.9698 278.9016 0062251  14.1102 346.1806 14.16151319 88376

Epoch: 2026-04-28T04:35Z

TLE epoch observation values (Epoch: 2026-04-28T04:35:14.463Z)

Latitude

-0.00004°

Longitude

-6.07866°

Altitude

797.829 km

Speed

7.477 km/s

True Right ascension

18h 35m 36s

True Declination

0° 00' 00"

Sunlit

Object was in daylight 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

05:04:15

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

880.26 km

Perigee altitude

790.45 km

Semi-major axis

7,213.492 km

Eccentricity

0.00623

Inclination

88.9698°

RAAN

278.9016°

Arg. of periapsis

14.1102°

True anomaly

346.00891°

Mean anomaly

346.1806°

Eccentric anomaly

346.09489°

Mean motion

3.54262 °/min

Orbital period

101.62 mins

BSTAR

0.00018406

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

QIANFAN-9, 60387

QIANFAN-18, 60396

QIANFAN-17, 60395

CZ-6A DEB, 61378 (Decayed)

CZ-6A DEB, 61392 (Decayed)

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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.
9 mins	2026-04-28 22:07:15.217Z	23.178° NE	2026-04-28 22:12:15.217Z	89.343° E	26.989°	2026-04-28 22:16:15.217Z	140.736° SSE
8 mins	2026-04-28 23:50:15.217Z	330.818° NNW	2026-04-28 23:53:15.217Z	286.154° WNW	28.404°	2026-04-28 23:58:15.217Z	219.182° SW
8 mins	2026-04-29 11:14:15.217Z	186.407° SSW	2026-04-29 11:18:15.217Z	313.811° NW	43.236°	2026-04-29 11:22:15.217Z	354.643° N

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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, 63391 on other resources

View CZ-6A DEB, 63391 on Heavens-Above

View CZ-6A DEB, 63391 on Keep Track

View CZ-6A DEB, 63391 on Celestrak

View CZ-6A DEB, 63391 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, 63391

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 17 hours ago

TLE from 17 hours ago

TLE epoch observation values (Epoch: 2026-04-28T04:35:14.463Z)

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, 63391 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 17 hours ago