CZ-6A DEB, 64645

Orbit data source: Space-Track

CZ-6A DEB, 64645 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/64645?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

64645, 2024-140AEK

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 (1 year 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)

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Last TLE update: 1 day ago

TLE from 1 day ago

0 CZ-6A DEB
1 64645U 24140AEK 25354.20324284  .00001581  00000-0  82726-3 0  9993
2 64645  88.3156 256.3067 0094818  63.7763 297.3131 14.11516279 61896

Epoch: 2025-12-20T04:52Z

TLE epoch observation values (Epoch: 2025-12-20T04:52:40.181Z)

Latitude

-0.00001°

Longitude

94.10586°

Altitude

826.269 km

Speed

7.456 km/s

True Right ascension

17h 05m 13s

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

05:18:48

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

919.702 km

Perigee altitude

782.609 km

Semi-major axis

7,229.293 km

Eccentricity

0.00948

Inclination

88.3156°

RAAN

256.3067°

Arg. of periapsis

63.7763°

True anomaly

296.34247°

Mean anomaly

297.3131°

Eccentric anomaly

296.82831°

Mean motion

3.53101 °/min

Orbital period

101.95 mins

BSTAR

0.00082726

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

CZ-6A DEB, 60743 (Decayed)

CZ-6A DEB, 61478 (Decayed)

CZ-6A DEB, 61130

CZ-6A DEB, 61342 (Decayed)

CZ-6A DEB, 61820 (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.
8 mins	2025-12-21 06:58:58.215Z	328.399° NNW	2025-12-21 07:02:58.215Z	275.725° WNW	21.968°	2025-12-21 07:06:58.215Z	229.405° WSW
4 mins	2025-12-21 16:46:58.215Z	90.516° ESE	2025-12-21 16:47:58.215Z	77.225° E	15.226°	2025-12-21 16:50:58.215Z	41.239° NE
8 mins	2025-12-21 18:25:58.215Z	199.575° SSW	2025-12-21 18:29:58.215Z	290.104° WNW	39.187°	2025-12-21 18:33:58.215Z	348.822° N
8 mins	2025-12-22 05:06:58.215Z	31.851° NE	2025-12-22 05:09:58.215Z	84.184° E	30.228°	2025-12-22 05:14:58.215Z	149.44° SSE

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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, 64645 on other resources

View CZ-6A DEB, 64645 on Heavens-Above

View CZ-6A DEB, 64645 on Keep Track

View CZ-6A DEB, 64645 on Celestrak

View CZ-6A DEB, 64645 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, 64645

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 1 day ago

TLE from 1 day ago

TLE epoch observation values (Epoch: 2025-12-20T04:52:40.181Z)

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, 64645 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 1 day ago