CZ-6A DEB, 61124

Orbit data source: Space-Track

CZ-6A DEB, 61124 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/61124?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

61124, 2024-140PS

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: 16 hours ago

TLE from 16 hours ago

0 CZ-6A DEB
1 61124U 24140PS  26118.40527911  .00002277  00000-0  26526-3 0  9994
2 61124  88.9941 273.8362 0174015   6.2842 354.0501 14.74507133 90424

Epoch: 2026-04-28T09:43Z

TLE epoch observation values (Epoch: 2026-04-28T09:43:36.115Z)

Latitude

-0.00008°

Longitude

-88.44534°

Altitude

528.26 km

Speed

7.664 km/s

True Right ascension

18h 15m 20s

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

09:13:31

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

765.777 km

Perigee altitude

521.4 km

Semi-major axis

7,021.725 km

Eccentricity

0.0174

Inclination

88.9941°

RAAN

273.8362°

Arg. of periapsis

6.2842°

True anomaly

353.83883°

Mean anomaly

354.0501°

Eccentric anomaly

353.94493°

Mean motion

3.68873 °/min

Orbital period

97.59 mins

BSTAR

0.00026526

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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.
6 mins	2026-04-29 10:16:50.414Z	148.739° SSE	2026-04-29 10:19:50.414Z	89.894° E	31.204°	2026-04-29 10:22:50.414Z	21.275° NNE
8 mins	2026-04-29 22:07:50.414Z	21.609° NNE	2026-04-29 22:10:50.414Z	77.245° E	35.308°	2026-04-29 22:15:50.414Z	160.026° S
5 mins	2026-04-29 23:46:50.414Z	306.091° NW	2026-04-29 23:48:50.414Z	275.722° WNW	17.816°	2026-04-29 23:51:50.414Z	239.052° WSW

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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, 61124 on Gunter's Space Page

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CZ-6A DEB, 61124

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 16 hours ago

TLE from 16 hours ago

TLE epoch observation values (Epoch: 2026-04-28T09:43:36.115Z)

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, 61124 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 16 hours ago