CZ-6A DEB, 60646

Orbit data source: Space-Track

CZ-6A DEB, 60646 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/60646?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

60646, 2024-140AX

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)

Expand to show TLE details & history
Last TLE update: 7 hours ago

TLE from 7 hours ago

0 CZ-6A DEB
1 60646U 24140AX  25346.28238945  .00013857  00000-0  25377-2 0  9994
2 60646  89.0072 292.8727 0081326 169.7364 190.5536 14.63598741 71479

Epoch: 2025-12-12T06:46Z

TLE epoch observation values (Epoch: 2025-12-12T06:46:38.448Z)

Latitude

0.00002°

Longitude

109.98625°

Altitude

741.164 km

Speed

7.454 km/s

True Right ascension

19h 31m 29s

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

12:19:39

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

735.855 km

Perigee altitude

621.078 km

Semi-major axis

7,056.603 km

Eccentricity

0.00813

Inclination

89.0072°

RAAN

292.8727°

Arg. of periapsis

169.7364°

True anomaly

190.3846°

Mean anomaly

190.5536°

Eccentric anomaly

190.46893°

Mean motion

3.66142 °/min

Orbital period

98.32 mins

BSTAR

0.0025377

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

CZ-6A DEB, 60629 (Decayed)

CZ-6A DEB, 60809 (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.
7 mins	2025-12-12 20:02:03.759Z	126.339° SE	2025-12-12 20:06:03.759Z	71.625° E	19.583°	2025-12-12 20:09:03.759Z	32.04° NE
7 mins	2025-12-12 21:41:03.759Z	218.505° SW	2025-12-12 21:44:03.759Z	282.179° WNW	31.351°	2025-12-12 21:48:03.759Z	341.214° N
4 mins	2025-12-13 08:00:03.759Z	54.585° ENE	2025-12-13 08:02:03.759Z	91.295° ESE	19.144°	2025-12-13 08:04:03.759Z	122.737° SE
5 mins	2025-12-13 09:38:03.759Z	320.976° NNW	2025-12-13 09:40:03.759Z	277.191° WNW	26.792°	2025-12-13 09:43:03.759Z	223.175° 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, 60646 on other resources

View CZ-6A DEB, 60646 on Heavens-Above

View CZ-6A DEB, 60646 on Keep Track

View CZ-6A DEB, 60646 on Celestrak

View CZ-6A DEB, 60646 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, 60646

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 7 hours ago

TLE from 7 hours ago

TLE epoch observation values (Epoch: 2025-12-12T06:46:38.448Z)

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, 60646 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 7 hours ago