CZ-6A DEB, 61492

Orbit data source: Space-Track

CZ-6A DEB, 61492 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/61492?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

61492, 2024-140ABA

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

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 14 hours ago

TLE from 14 hours ago

0 CZ-6A DEB
1 61492U 24140ABA 26171.24441469  .00002051  00000-0  40870-3 0  9994
2 61492  88.9934 269.2243 0124399 270.5325  88.1633 14.56858137 94128

Epoch: 2026-06-20T05:51Z

TLE epoch observation values (Epoch: 2026-06-20T05:51:57.429Z)

Latitude

0.00003°

Longitude

-87.22681°

Altitude

704.714 km

Speed

7.504 km/s

True Right ascension

17h 56m 53s

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

07:14:25

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

788.289 km

Perigee altitude

612.181 km

Semi-major axis

7,078.372 km

Eccentricity

0.01244

Inclination

88.9934°

RAAN

269.2243°

Arg. of periapsis

270.5325°

True anomaly

89.58864°

Mean anomaly

88.1633°

Eccentric anomaly

88.87592°

Mean motion

3.64454 °/min

Orbital period

98.78 mins

BSTAR

0.0004087

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

CZ-6A DEB, 60882

CZ-6A DEB, 61384 (Decayed)

CZ-6A DEB, 61344 (Decayed)

CZ-6A DEB, 60711

CZ-6A DEB, 61310 (Decayed)

QIANFAN-4, 60382

QIANFAN-5, 60383

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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	2026-06-21 06:42:40.627Z	163.562° S	2026-06-21 06:46:40.627Z	84.311° E	41.856°	2026-06-21 06:51:40.627Z	5.802° NNE
8 mins	2026-06-21 18:43:40.627Z	5.681° NNE	2026-06-21 18:46:40.627Z	39.18° NE	43.612°	2026-06-21 18:51:40.627Z	177.349° S

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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, 61492 on other resources

View CZ-6A DEB, 61492 on Heavens-Above

View CZ-6A DEB, 61492 on Keep Track

View CZ-6A DEB, 61492 on Celestrak

View CZ-6A DEB, 61492 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, 61492

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 14 hours ago

TLE from 14 hours ago

TLE epoch observation values (Epoch: 2026-06-20T05:51:57.429Z)

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, 61492 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 14 hours ago