CZ-6A DEB, 61403

Orbit data source: Space-Track

CZ-6A DEB, 61403 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/61403?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

61403, 2024-140XU

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, 1.1 m

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 6 days ago

TLE from 6 days ago

0 CZ-6A DEB
1 61403U 24140XU  26108.43601011  .00001486  00000-0  60848-3 0  9996
2 61403  88.9455 277.1915 0032901  17.4717 342.7600 14.26430207 83461

Epoch: 2026-04-18T10:27Z

TLE epoch observation values (Epoch: 2026-04-18T10:27:51.273Z)

Latitude

-0.00005°

Longitude

-86.32702°

Altitude

784.185 km

Speed

7.473 km/s

True Right ascension

18h 28m 45s

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

12:55:05

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

824.249 km

Perigee altitude

777.011 km

Semi-major axis

7,178.767 km

Eccentricity

0.00329

Inclination

88.9455°

RAAN

277.1915°

Arg. of periapsis

17.4717°

True anomaly

342.64782°

Mean anomaly

342.76°

Eccentric anomaly

342.70395°

Mean motion

3.56836 °/min

Orbital period

100.89 mins

BSTAR

0.00060848

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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	2026-04-24 11:22:27.173Z	183.893° SSW	2026-04-24 11:26:27.173Z	302.975° NW	44.226°	2026-04-24 11:31:27.173Z	356.637° N
6 mins	2026-04-24 21:57:27.173Z	44.021° NE	2026-04-24 22:00:27.173Z	84.701° E	19.237°	2026-04-24 22:03:27.173Z	122.072° SE
9 mins	2026-04-24 23:37:27.173Z	343.218° N	2026-04-24 23:41:27.173Z	272.152° WNW	35.964°	2026-04-24 23:46:27.173Z	204.751° 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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View CZ-6A DEB, 61403 on Celestrak

View CZ-6A DEB, 61403 on Gunter's Space Page

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CZ-6A DEB, 61403

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 6 days ago

TLE from 6 days ago

TLE epoch observation values (Epoch: 2026-04-18T10:27:51.273Z)

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, 61403 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 6 days ago