CZ-6A DEB, 61081

Orbit data source: Space-Track

CZ-6A DEB, 61081 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/61081?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

61081, 2024-140MX

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 61081U 24140MX  26130.14866793  .00001733  00000-0  30689-3 0  9996
2 61081  88.9774 272.5607 0112915  11.1312 349.2359 14.62736530 90717

Epoch: 2026-05-10T03:34Z

TLE epoch observation values (Epoch: 2026-05-10T03:34:04.909Z)

Latitude

-0.00002°

Longitude

-8.91566°

Altitude

609.138 km

Speed

7.596 km/s

True Right ascension

18h 10m 14s

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

21:27:34

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

760.952 km

Perigee altitude

601.531 km

Semi-major axis

7,059.379 km

Eccentricity

0.01129

Inclination

88.9774°

RAAN

272.5607°

Arg. of periapsis

11.1312°

True anomaly

348.99085°

Mean anomaly

349.2359°

Eccentric anomaly

349.11372°

Mean motion

3.65926 °/min

Orbital period

98.38 mins

BSTAR

0.00030689

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

CZ-6A DEB, 61344 (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.
5 mins	2026-05-10 20:34:37.948Z	49.875° ENE	2026-05-10 20:36:37.948Z	76.411° E	15.605°	2026-05-10 20:39:37.948Z	115.122° SE
7 mins	2026-05-10 22:12:37.948Z	342.304° N	2026-05-10 22:15:37.948Z	273.262° WNW	38.188°	2026-05-10 22:19:37.948Z	202.941° SW
6 mins	2026-05-11 09:15:37.948Z	132.967° SE	2026-05-11 09:17:37.948Z	94.54° ESE	27.233°	2026-05-11 09:21:37.948Z	21.398° NNE
5 mins	2026-05-11 10:54:37.948Z	245.222° WSW	2026-05-11 10:56:37.948Z	278.912° WNW	18.068°	2026-05-11 10:59:37.948Z	323.6° NNW

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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, 61081 on other resources

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View CZ-6A DEB, 61081 on Keep Track

View CZ-6A DEB, 61081 on Celestrak

View CZ-6A DEB, 61081 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, 61081

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: 2026-05-10T03:34:04.909Z)

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, 61081 on other resources

Documentation

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