CZ-6A DEB, 61086

Orbit data source: Space-Track

CZ-6A DEB, 61086 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/61086?theme=dark&initialShowStats=false

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ISO8601 Format

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ISO8601 Format

Identifier

61086, 2024-140NC

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, 0.2 m

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 15 hours ago

TLE from 15 hours ago

0 CZ-6A DEB
1 61086U 24140NC  26113.70157103  .00002978  00000-0  24368-3 0  9991
2 61086  89.0264 276.0484 0184449 356.7974   3.2055 14.86609420 89545

Epoch: 2026-04-23T16:50Z

TLE epoch observation values (Epoch: 2026-04-23T16:50:15.736Z)

Latitude

-0.00004°

Longitude

171.73797°

Altitude

483 km

Speed

7.694 km/s

True Right ascension

18h 24m 11s

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

14:41:41

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

734.204 km

Perigee altitude

476.583 km

Semi-major axis

6,983.53 km

Eccentricity

0.01844

Inclination

89.0264°

RAAN

276.0484°

Arg. of periapsis

356.7974°

True anomaly

3.32647°

Mean anomaly

3.2055°

Eccentric anomaly

3.2657°

Mean motion

3.71904 °/min

Orbital period

96.8 mins

BSTAR

0.00024368

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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	2026-04-24 10:43:45.804Z	147.646° SSE	2026-04-24 10:46:45.804Z	90.262° ESE	29.244°	2026-04-24 10:49:45.804Z	22.298° NNE
7 mins	2026-04-24 22:29:45.804Z	31.964° NE	2026-04-24 22:32:45.804Z	97.383° ESE	31.024°	2026-04-24 22:36:45.804Z	153.125° SSE
5 mins	2026-04-25 00:06:45.804Z	316.368° NNW	2026-04-25 00:08:45.804Z	285.246° WNW	20.443°	2026-04-25 00:11:45.804Z	240.206° 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, 61086 on Gunter's Space Page

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CZ-6A DEB, 61086

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 15 hours ago

TLE from 15 hours ago

TLE epoch observation values (Epoch: 2026-04-23T16:50:15.736Z)

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, 61086 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 15 hours ago