CZ-6A DEB, 61326

Orbit data source: Space-Track

CZ-6A DEB, 61326 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/61326?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

61326, 2024-140UP

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: 8 hours ago

TLE from 8 hours ago

0 CZ-6A DEB
1 61326U 24140UP  26118.45891023  .00004842  00000-0  77190-3 0  9994
2 61326  89.1857 290.1768 0118384  45.7092 315.3760 14.67160627 88026

Epoch: 2026-04-28T11:00Z

TLE epoch observation values (Epoch: 2026-04-28T11:00:49.843Z)

Latitude

-0.00003°

Longitude

-91.4648°

Altitude

614.362 km

Speed

7.583 km/s

True Right ascension

19h 20m 42s

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

02:16:30

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

750.433 km

Perigee altitude

583.626 km

Semi-major axis

7,045.166 km

Eccentricity

0.01184

Inclination

89.1857°

RAAN

290.1768°

Arg. of periapsis

45.7092°

True anomaly

314.41297°

Mean anomaly

315.376°

Eccentric anomaly

314.8955°

Mean motion

3.67034 °/min

Orbital period

98.08 mins

BSTAR

0.0007719

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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.
8 mins	2026-04-28 23:01:57.993Z	24.857° NE	2026-04-28 23:05:57.993Z	88.572° E	26.372°	2026-04-28 23:09:57.993Z	146.443° SSE
5 mins	2026-04-29 00:41:57.993Z	313.805° NW	2026-04-29 00:43:57.993Z	276.896° WNW	22.285°	2026-04-29 00:46:57.993Z	231.773° WSW
6 mins	2026-04-29 11:41:57.993Z	166.689° S	2026-04-29 11:44:57.993Z	53.562° ENE	42.559°	2026-04-29 11:47:57.993Z	5.081° NNE

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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, 61326 on Gunter's Space Page

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CZ-6A DEB, 61326

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 8 hours ago

TLE from 8 hours ago

TLE epoch observation values (Epoch: 2026-04-28T11:00:49.843Z)

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, 61326 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 8 hours ago