CZ-6A DEB, 61393

Orbit data source: Space-Track

CZ-6A DEB, 61393 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/61393?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

61393, 2024-140XJ

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: 10 hours ago

TLE from 10 hours ago

0 CZ-6A DEB
1 61393U 24140XJ  26118.44558978  .00002273  00000-0  11369-2 0  9997
2 61393  88.9917 280.8171 0085512  25.2935 335.2401 14.14552710 84684

Epoch: 2026-04-28T10:41Z

TLE epoch observation values (Epoch: 2026-04-28T10:41:38.956Z)

Latitude

-0.00003°

Longitude

-96.01601°

Altitude

790.882 km

Speed

7.487 km/s

True Right ascension

18h 43m 16s

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

03:47:44

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

902.523 km

Perigee altitude

779.062 km

Semi-major axis

7,218.93 km

Eccentricity

0.00855

Inclination

88.9917°

RAAN

280.8171°

Arg. of periapsis

25.2935°

True anomaly

334.82569°

Mean anomaly

335.2401°

Eccentric anomaly

335.0333°

Mean motion

3.53862 °/min

Orbital period

101.73 mins

BSTAR

0.0011369

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

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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 23:09:57.185Z	0.185° NNE	2026-04-28 23:13:57.185Z	252.924° W	44.971°	2026-04-28 23:18:57.185Z	183.712° SSW
7 mins	2026-04-29 10:35:57.185Z	138.21° SSE	2026-04-29 10:38:57.185Z	82.48° E	31.978°	2026-04-29 10:42:57.185Z	19.172° NNE
6 mins	2026-04-29 12:17:57.185Z	237.369° WSW	2026-04-29 12:20:57.185Z	280.165° WNW	20.825°	2026-04-29 12:23:57.185Z	321.712° NNW

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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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View CZ-6A DEB, 61393 on Gunter's Space Page

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CZ-6A DEB, 61393

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 10 hours ago

TLE from 10 hours ago

TLE epoch observation values (Epoch: 2026-04-28T10:41:38.956Z)

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, 61393 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 10 hours ago