CZ-6A DEB, 61125

Orbit data source: Space-Track

CZ-6A DEB, 61125 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/61125?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

61125, 2024-140PT

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: 9 hours ago

TLE from 9 hours ago

0 CZ-6A DEB
1 61125U 24140PT  26114.39392022  .00000379  00000-0  18622-3 0  9991
2 61125  88.8476 270.6555 0070827  26.3099 334.1656 14.14267864 86310

Epoch: 2026-04-24T09:27Z

TLE epoch observation values (Epoch: 2026-04-24T09:27:14.707Z)

Latitude

-0.00007°

Longitude

-83.58306°

Altitude

801.863 km

Speed

7.476 km/s

True Right ascension

18h 02m 37s

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

01:39:01

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

892.9 km

Perigee altitude

790.628 km

Semi-major axis

7,219.901 km

Eccentricity

0.00708

Inclination

88.8476°

RAAN

270.6555°

Arg. of periapsis

26.3099°

True anomaly

333.80908°

Mean anomaly

334.1656°

Eccentric anomaly

333.98763°

Mean motion

3.53791 °/min

Orbital period

101.76 mins

BSTAR

0.00018622

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

CZ-6A DEB, 60629 (Decayed)

CZ-6A DEB, 61392 (Decayed)

CZ-6A DEB, 60851 (Decayed)

CZ-6A DEB, 61795 (Decayed)

CZ-6A DEB, 61433 (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.
9 mins	2026-04-24 21:55:18.595Z	23.545° NE	2026-04-24 21:59:18.595Z	76.849° E	29.13°	2026-04-24 22:04:18.595Z	146.264° SSE
7 mins	2026-04-24 23:38:18.595Z	325.932° NNW	2026-04-24 23:41:18.595Z	280.311° WNW	26.34°	2026-04-24 23:45:18.595Z	226.675° WSW
8 mins	2026-04-25 11:03:18.595Z	193.013° SSW	2026-04-25 11:06:18.595Z	250.076° W	42.253°	2026-04-25 11:11:18.595Z	352.655° N

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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, 61125 on other resources

View CZ-6A DEB, 61125 on Heavens-Above

View CZ-6A DEB, 61125 on Keep Track

View CZ-6A DEB, 61125 on Celestrak

View CZ-6A DEB, 61125 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, 61125

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 9 hours ago

TLE from 9 hours ago

TLE epoch observation values (Epoch: 2026-04-24T09:27:14.707Z)

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, 61125 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 9 hours ago