CZ-6A DEB, 61111

Orbit data source: Space-Track

CZ-6A DEB, 61111 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/61111?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

61111, 2024-140PD

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

Medium (>0.1 m² and <1 m²)

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

TLE from 16 hours ago

0 CZ-6A DEB
1 61111U 24140PD  26171.24372885  .00000356  00000-0  11358-3 0  9992
2 61111  88.9023 264.1368 0066590   4.7204 355.4608 14.36446219 93929

Epoch: 2026-06-20T05:50Z

TLE epoch observation values (Epoch: 2026-06-20T05:50:58.172Z)

Latitude

-0.00004°

Longitude

-92.06673°

Altitude

725.881 km

Speed

7.517 km/s

True Right ascension

17h 36m 32s

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

08:32:41

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

814.773 km

Perigee altitude

719.612 km

Semi-major axis

7,145.329 km

Eccentricity

0.00666

Inclination

88.9023°

RAAN

264.1368°

Arg. of periapsis

4.7204°

True anomaly

355.39991°

Mean anomaly

355.4608°

Eccentric anomaly

355.4304°

Mean motion

3.59343 °/min

Orbital period

100.18 mins

BSTAR

0.00011358

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

CZ-6A DEB, 61384 (Decayed)

CZ-6A DEB, 60777 (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	2026-06-21 05:24:43.355Z	104.167° ESE	2026-06-21 05:26:43.355Z	77.491° E	15.427°	2026-06-21 05:29:43.355Z	39.594° NE
7 mins	2026-06-21 07:03:43.355Z	205.85° SW	2026-06-21 07:06:43.355Z	277.707° WNW	37.692°	2026-06-21 07:10:43.355Z	345.948° N
6 mins	2026-06-21 17:33:43.355Z	42.633° NE	2026-06-21 17:36:43.355Z	92.113° ESE	23.949°	2026-06-21 17:39:43.355Z	132.492° SE
7 mins	2026-06-21 19:13:43.355Z	328.035° NNW	2026-06-21 19:16:43.355Z	272.507° WNW	29.576°	2026-06-21 19:20:43.355Z	217.677° SW

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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, 61111 on other resources

View CZ-6A DEB, 61111 on Heavens-Above

View CZ-6A DEB, 61111 on Keep Track

View CZ-6A DEB, 61111 on Celestrak

View CZ-6A DEB, 61111 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, 61111

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: 2026-06-20T05:50:58.172Z)

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, 61111 on other resources

Documentation

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