CZ-6A DEB, 61085

Orbit data source: Space-Track

CZ-6A DEB, 61085 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/61085?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

61085, 2024-140NB

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: 10 hours ago

TLE from 10 hours ago

0 CZ-6A DEB
1 61085U 24140NB  26114.46419490  .00000404  00000-0  18592-3 0  9998
2 61085  89.1355 291.2046 0050414   5.8342 354.3423 14.18632941 85885

Epoch: 2026-04-24T11:08Z

TLE epoch observation values (Epoch: 2026-04-24T11:08:26.439Z)

Latitude

-0.00006°

Longitude

-88.40211°

Altitude

796.864 km

Speed

7.474 km/s

True Right ascension

19h 24m 49s

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

04:22:50

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

863.256 km

Perigee altitude

790.609 km

Semi-major axis

7,205.069 km

Eccentricity

0.00504

Inclination

89.1355°

RAAN

291.2046°

Arg. of periapsis

5.8342°

True anomaly

354.28499°

Mean anomaly

354.3423°

Eccentric anomaly

354.31368°

Mean motion

3.54884 °/min

Orbital period

101.44 mins

BSTAR

0.00018592

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

CZ-6A DEB, 60819

CZ-6A DEB, 60629 (Decayed)

CZ-6A DEB, 61392 (Decayed)

CZ-6A DEB, 60851 (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.
10 mins	2026-04-24 23:33:40.763Z	14.029° NNE	2026-04-24 23:38:40.763Z	83.67° E	36.223°	2026-04-24 23:43:40.763Z	158.941° S
6 mins	2026-04-25 01:17:40.763Z	313.475° NW	2026-04-25 01:19:40.763Z	286.053° WNW	20.11°	2026-04-25 01:23:40.763Z	237.718° WSW
6 mins	2026-04-25 10:59:40.763Z	108.575° ESE	2026-04-25 11:01:40.763Z	82.169° E	18.183°	2026-04-25 11:05:40.763Z	32.652° NE
8 mins	2026-04-25 12:39:40.763Z	206.664° SW	2026-04-25 12:42:40.763Z	256.996° W	35.758°	2026-04-25 12:47:40.763Z	344.819° N

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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, 61085 on other resources

View CZ-6A DEB, 61085 on Heavens-Above

View CZ-6A DEB, 61085 on Keep Track

View CZ-6A DEB, 61085 on Celestrak

View CZ-6A DEB, 61085 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, 61085

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 10 hours ago

TLE from 10 hours ago

TLE epoch observation values (Epoch: 2026-04-24T11:08:26.439Z)

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, 61085 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 10 hours ago