CZ-6A DEB, 63390

Orbit data source: Space-Track

CZ-6A DEB, 63390 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/63390?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

63390, 2024-140ADM

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: 11 hours ago

TLE from 11 hours ago

0 CZ-6A DEB
1 63390U 24140ADM 26118.70299855  .00001258  00000-0  58860-3 0  9991
2 63390  88.9997 280.7881 0053439 355.1337   4.9325 14.18962514 88435

Epoch: 2026-04-28T16:52Z

TLE epoch observation values (Epoch: 2026-04-28T16:52:19.074Z)

Latitude

-0.0001°

Longitude

171.03411°

Altitude

793.538 km

Speed

7.477 km/s

True Right ascension

18h 43m 09s

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

11:00:38

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

864.313 km

Perigee altitude

787.319 km

Semi-major axis

7,203.953 km

Eccentricity

0.00534

Inclination

88.9997°

RAAN

280.7881°

Arg. of periapsis

355.1337°

True anomaly

4.98551°

Mean anomaly

4.9325°

Eccentric anomaly

4.95897°

Mean motion

3.54966 °/min

Orbital period

101.42 mins

BSTAR

0.0005886

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

CZ-6A DEB, 61460 (Decayed)

CZ-6A DEB, 60869 (Decayed)

CZ-6A DEB, 61812

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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.
6 mins	2026-04-29 09:56:39.737Z	110.284° ESE	2026-04-29 09:59:39.737Z	73.166° E	16.379°	2026-04-29 10:02:39.737Z	37.724° NE
9 mins	2026-04-29 11:36:39.737Z	199.648° SSW	2026-04-29 11:40:39.737Z	281.367° WNW	38.847°	2026-04-29 11:45:39.737Z	349.676° N
8 mins	2026-04-29 22:14:39.737Z	32.918° NE	2026-04-29 22:17:39.737Z	78.463° E	27.961°	2026-04-29 22:22:39.737Z	145.115° SSE
8 mins	2026-04-29 23:55:39.737Z	332.539° NNW	2026-04-29 23:59:39.737Z	272.219° WNW	27.317°	2026-04-30 00:03:39.737Z	222.404° SW

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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, 63390 on other resources

View CZ-6A DEB, 63390 on Heavens-Above

View CZ-6A DEB, 63390 on Keep Track

View CZ-6A DEB, 63390 on Celestrak

View CZ-6A DEB, 63390 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, 63390

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 11 hours ago

TLE from 11 hours ago

TLE epoch observation values (Epoch: 2026-04-28T16:52:19.074Z)

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, 63390 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 11 hours ago