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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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 (1 year 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: 6 hours ago

TLE from 6 hours ago

0 CZ-6A DEB
1 61126U 24140PU  25351.33758219  .00012136  00000-0  73944-3 0  9994
2 61126  89.1531 298.5874 0204546  37.4969 324.0329 14.94394626 71826

Epoch: 2025-12-17T08:06Z

TLE epoch observation values (Epoch: 2025-12-17T08:06:07.101Z)

Latitude

0.00004°

Longitude

90.84893°

Altitude

473.154 km

Speed

7.692 km/s

True Right ascension

19h 54m 20s

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

12:46:21

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

723.443 km

Perigee altitude

438.747 km

Semi-major axis

6,959.232 km

Eccentricity

0.02045

Inclination

89.1531°

RAAN

298.5874°

Arg. of periapsis

37.4969°

True anomaly

322.62734°

Mean anomaly

324.0329°

Eccentric anomaly

323.33305°

Mean motion

3.73853 °/min

Orbital period

96.29 mins

BSTAR

0.00073944

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

CZ-6A DEB, 61496 (Decayed)

CZ-6A DEB, 60640 (Decayed)

CZ-6A DEB, 61830 (Decayed)

CZ-6A DEB, 61802 (Decayed)

CZ-6A DEB, 61324 (Decayed)

CZ-6A DEB, 61397 (Decayed)

CZ-6A DEB, 61379 (Decayed)

CZ-6A DEB, 61378 (Decayed)

QIANFAN-17, 60395

QIANFAN-18, 60396

CZ-6A DEB, 61091 (Decayed)

QIANFAN-9, 60387

QIANFAN-1, 60379

CZ-6A DEB, 61797 (Decayed)

CZ-6A DEB, 60835 (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.
6 mins	2025-12-17 21:05:00.985Z	174.712° S	2025-12-17 21:08:00.985Z	25.224° NE	43.756°	2025-12-17 21:11:00.985Z	0.697° NNE
7 mins	2025-12-18 08:46:00.985Z	12.311° NNE	2025-12-18 08:49:00.985Z	90.474° ESE	41.584°	2025-12-18 08:53:00.985Z	170.422° 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, 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: 6 hours ago

TLE from 6 hours ago

TLE epoch observation values (Epoch: 2025-12-17T08:06:07.101Z)

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: 6 hours ago