CZ-6A DEB, 61126

Orbit data source: Space-Track

CZ-6A DEB, 61126 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/61126?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

61126, 2024-140PU

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: 14 hours ago

TLE from 14 hours ago

0 CZ-6A DEB
1 61126U 24140PU  26171.28409969  .00008768  00000-0  49550-3 0  9996
2 61126  89.1501 278.4036 0193070  77.8109 284.4675 14.98417100 99485

Epoch: 2026-06-20T06:49Z

TLE epoch observation values (Epoch: 2026-06-20T06:49:06.213Z)

Latitude

-0.00005°

Longitude

-92.37322°

Altitude

543.869 km

Speed

7.607 km/s

True Right ascension

18h 33m 36s

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

07:24:44

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

702.745 km

Perigee altitude

434.503 km

Semi-major axis

6,946.761 km

Eccentricity

0.01931

Inclination

89.1501°

RAAN

278.4036°

Arg. of periapsis

77.8109°

True anomaly

282.31275°

Mean anomaly

284.4675°

Eccentric anomaly

283.39137°

Mean motion

3.7486 °/min

Orbital period

96.04 mins

BSTAR

0.0004955

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

CZ-6A DEB, 60882

CZ-6A DEB, 61384 (Decayed)

CZ-6A DEB, 60744 (Decayed)

CZ-6A DEB, 60849

CZ-6A DEB, 60885

CZ-6A DEB, 61344 (Decayed)

CZ-6A DEB, 60711

CZ-6A DEB, 60799

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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.
4 mins	2026-06-21 06:59:57.652Z	132.729° SE	2026-06-21 07:01:57.652Z	87.846° E	23.803°	2026-06-21 07:03:57.652Z	36.915° NE
4 mins	2026-06-21 20:15:57.652Z	302.598° NW	2026-06-21 20:16:57.652Z	279.416° WNW	20.645°	2026-06-21 20:19:57.652Z	227.269° 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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Check out CZ-6A DEB, 61126 on other resources

View CZ-6A DEB, 61126 on Heavens-Above

View CZ-6A DEB, 61126 on Keep Track

View CZ-6A DEB, 61126 on Celestrak

View CZ-6A DEB, 61126 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, 61126

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 14 hours ago

TLE from 14 hours ago

TLE epoch observation values (Epoch: 2026-06-20T06:49:06.213Z)

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, 61126 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 14 hours ago