CZ-6A DEB, 61120

Orbit data source: Space-Track

CZ-6A DEB, 61120 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/61120?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

61120, 2024-140PN

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 61120U 24140PN  26118.48341522  .00001624  00000-0  84789-3 0  9990
2 61120  88.9863 280.5944 0090172  26.7154 333.8635 14.11941091 87007

Epoch: 2026-04-28T11:36Z

TLE epoch observation values (Epoch: 2026-04-28T11:36:07.075Z)

Latitude

0.00005°

Longitude

-109.89316°

Altitude

797.346 km

Speed

7.485 km/s

True Right ascension

18h 42m 22s

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

03:42:09

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

914.874 km

Perigee altitude

784.525 km

Semi-major axis

7,227.836 km

Eccentricity

0.00902

Inclination

88.9863°

RAAN

280.5944°

Arg. of periapsis

26.7154°

True anomaly

333.40368°

Mean anomaly

333.8635°

Eccentric anomaly

333.63406°

Mean motion

3.53208 °/min

Orbital period

101.92 mins

BSTAR

0.00084789

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

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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	2026-04-28 22:23:23.044Z	22.945° NE	2026-04-28 22:27:23.044Z	78.823° E	30.955°	2026-04-28 22:32:23.044Z	149.146° SSE
7 mins	2026-04-29 00:06:23.044Z	325.02° NNW	2026-04-29 00:09:23.044Z	281.436° WNW	25.126°	2026-04-29 00:13:23.044Z	229.417° WSW
4 mins	2026-04-29 09:53:23.044Z	89.443° E	2026-04-29 09:54:23.044Z	76.409° E	14.762°	2026-04-29 09:57:23.044Z	40.856° NE
8 mins	2026-04-29 11:32:23.044Z	197.475° SSW	2026-04-29 11:36:23.044Z	295.639° NW	39.635°	2026-04-29 11:40:23.044Z	349.178° 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, 61120 on other resources

View CZ-6A DEB, 61120 on Heavens-Above

View CZ-6A DEB, 61120 on Keep Track

View CZ-6A DEB, 61120 on Celestrak

View CZ-6A DEB, 61120 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, 61120

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: 2026-04-28T11:36:07.075Z)

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, 61120 on other resources

Documentation

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