CZ-6A DEB, 61161

Orbit data source: Space-Track

CZ-6A DEB, 61161 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/61161?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

61161, 2024-140RF

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: 16 hours ago

TLE from 16 hours ago

0 CZ-6A DEB
1 61161U 24140RF  26118.37652674  .00005530  00000-0  10119-2 0  9991
2 61161  88.8215 262.2531 0130556  96.4086 265.2012 14.60282334 89405

Epoch: 2026-04-28T09:02Z

TLE epoch observation values (Epoch: 2026-04-28T09:02:11.910Z)

Latitude

-0.00003°

Longitude

-89.64925°

Altitude

704.292 km

Speed

7.499 km/s

True Right ascension

17h 29m 00s

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

08:20:08

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

781.424 km

Perigee altitude

596.889 km

Semi-major axis

7,067.294 km

Eccentricity

0.01306

Inclination

88.8215°

RAAN

262.2531°

Arg. of periapsis

96.4086°

True anomaly

263.71258°

Mean anomaly

265.2012°

Eccentric anomaly

264.45667°

Mean motion

3.65312 °/min

Orbital period

98.55 mins

BSTAR

0.0010119

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

CZ-6A DEB, 61392 (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.
7 mins	2026-04-29 09:49:36.027Z	168.199° S	2026-04-29 09:53:36.027Z	48.492° ENE	41.978°	2026-04-29 09:56:36.027Z	6.114° NNE
7 mins	2026-04-29 21:47:36.027Z	2.84° NNE	2026-04-29 21:50:36.027Z	51.242° ENE	44.79°	2026-04-29 21:54:36.027Z	179.729° 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, 61161 on other resources

View CZ-6A DEB, 61161 on Heavens-Above

View CZ-6A DEB, 61161 on Keep Track

View CZ-6A DEB, 61161 on Celestrak

View CZ-6A DEB, 61161 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, 61161

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 16 hours ago

TLE from 16 hours ago

TLE epoch observation values (Epoch: 2026-04-28T09:02:11.910Z)

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, 61161 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 16 hours ago