CZ-6A DEB, 61436

Orbit data source: Space-Track

CZ-6A DEB, 61436 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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https://www.satcat.com/sats-embedded/61436?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

61436, 2024-140ZD

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: 1 day ago

TLE from 1 day ago

0 CZ-6A DEB
1 61436U 24140ZD  26113.48515687  .00000704  00000-0  32640-3 0  9997
2 61436  88.9352 276.6766 0057071   1.3728 358.7608 14.18858814 86399

Epoch: 2026-04-23T11:38Z

TLE epoch observation values (Epoch: 2026-04-23T11:38:37.553Z)

Latitude

0.00005°

Longitude

-109.51143°

Altitude

791.134 km

Speed

7.479 km/s

True Right ascension

18h 26m 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

21:33:28

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

867.284 km

Perigee altitude

785.052 km

Semi-major axis

7,204.305 km

Eccentricity

0.00571

Inclination

88.9352°

RAAN

276.6766°

Arg. of periapsis

1.3728°

True anomaly

358.74656°

Mean anomaly

358.7608°

Eccentric anomaly

358.75369°

Mean motion

3.5494 °/min

Orbital period

101.43 mins

BSTAR

0.0003264

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

CZ-6A DEB, 61798

CZ-6A DEB, 61353 (Decayed)

CZ-6A DEB, 61465 (Decayed)

CZ-6A DEB, 60629 (Decayed)

CZ-6A DEB, 61392 (Decayed)

CZ-6A DEB, 60851 (Decayed)

QIANFAN-16, 60394

CZ-6A DEB, 61795 (Decayed)

CZ-6A DEB, 61433 (Decayed)

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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 22:04:25.284Z	27.322° NE	2026-04-24 22:08:25.284Z	73.806° E	23.014°	2026-04-24 22:13:25.284Z	136.312° SSE
9 mins	2026-04-24 23:46:25.284Z	339.896° N	2026-04-24 23:50:25.284Z	278.842° WNW	32.643°	2026-04-24 23:55:25.284Z	211.533° SW
9 mins	2026-04-25 11:09:25.284Z	175.297° S	2026-04-25 11:13:25.284Z	36.547° NE	44.779°	2026-04-25 11:18:25.284Z	0.312° 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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Check out CZ-6A DEB, 61436 on other resources

View CZ-6A DEB, 61436 on Heavens-Above

View CZ-6A DEB, 61436 on Keep Track

View CZ-6A DEB, 61436 on Celestrak

View CZ-6A DEB, 61436 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, 61436

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 1 day ago

TLE from 1 day ago

TLE epoch observation values (Epoch: 2026-04-23T11:38:37.553Z)

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, 61436 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 1 day ago