CZ-6A DEB, 61365

Orbit data source: Space-Track

CZ-6A DEB, 61365 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/61365?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

61365, 2024-140WE

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: 15 hours ago

TLE from 15 hours ago

0 CZ-6A DEB
1 61365U 24140WE  26171.33568932  .00001553  00000-0  20547-3 0  9993
2 61365  89.1230 278.4286 0170513 160.7461 200.0308 14.69656139 95990

Epoch: 2026-06-20T08:03Z

TLE epoch observation values (Epoch: 2026-06-20T08:03:23.557Z)

Latitude

-0.00007°

Longitude

-110.97134°

Altitude

778.337 km

Speed

7.405 km/s

True Right ascension

18h 33m 42s

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

10:17:10

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

779.038 km

Perigee altitude

539.051 km

Semi-major axis

7,037.181 km

Eccentricity

0.01705

Inclination

89.123°

RAAN

278.4286°

Arg. of periapsis

160.7461°

True anomaly

199.37469°

Mean anomaly

200.0308°

Eccentric anomaly

199.70145°

Mean motion

3.67659 °/min

Orbital period

97.92 mins

BSTAR

0.00020547

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

CZ-6A DEB, 61384 (Decayed)

CZ-6A DEB, 61344 (Decayed)

CZ-6A DEB, 60710

CZ-6A DEB, 60782 (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	2026-06-21 07:02:55.689Z	152.183° SSE	2026-06-21 07:06:55.689Z	96.302° ESE	33.54°	2026-06-21 07:10:55.689Z	17.857° NNE
5 mins	2026-06-21 08:42:55.689Z	242.809° WSW	2026-06-21 08:44:55.689Z	270.349° WNW	17.84°	2026-06-21 08:47:55.689Z	314.622° NW
6 mins	2026-06-21 18:57:55.689Z	27.545° NE	2026-06-21 19:00:55.689Z	104.478° ESE	29.668°	2026-06-21 19:03:55.689Z	154.099° 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, 61365 on other resources

View CZ-6A DEB, 61365 on Heavens-Above

View CZ-6A DEB, 61365 on Keep Track

View CZ-6A DEB, 61365 on Celestrak

View CZ-6A DEB, 61365 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, 61365

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: 2026-06-20T08:03:23.557Z)

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, 61365 on other resources

Documentation

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