CZ-6A DEB, 61121

Orbit data source: Space-Track

CZ-6A DEB, 61121 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/61121?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

61121, 2024-140PP

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: 20 hours ago

TLE from 20 hours ago

0 CZ-6A DEB
1 61121U 24140PP  26054.33707176  .00000630  00000-0  19102-3 0  9998
2 61121  88.9406 281.6792 0073407  10.3420 349.9269 14.39531254 79560

Epoch: 2026-02-23T08:05Z

TLE epoch observation values (Epoch: 2026-02-23T08:05:23.000Z)

Latitude

-0.00009°

Longitude

7.10096°

Altitude

711.538 km

Speed

7.527 km/s

True Right ascension

18h 46m 43s

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

07:22:26

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

809.348 km

Perigee altitude

704.594 km

Semi-major axis

7,135.108 km

Eccentricity

0.00734

Inclination

88.9406°

RAAN

281.6792°

Arg. of periapsis

10.342°

True anomaly

349.77843°

Mean anomaly

349.9269°

Eccentric anomaly

349.8528°

Mean motion

3.60116 °/min

Orbital period

99.97 mins

BSTAR

0.00019102

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

CZ-6A DEB, 61279

CZ-6A DEB, 61495 (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	2026-02-24 04:41:41.741Z	320.352° NNW	2026-02-24 04:44:41.741Z	283.981° WNW	16.134°	2026-02-24 04:47:41.741Z	247.935° W
4 mins	2026-02-24 14:16:41.741Z	102.215° ESE	2026-02-24 14:18:41.741Z	74.111° E	15.688°	2026-02-24 14:20:41.741Z	46.976° ENE
8 mins	2026-02-24 15:54:41.741Z	203.621° SW	2026-02-24 15:57:41.741Z	254.751° W	35.935°	2026-02-24 16:02:41.741Z	346.902° N
7 mins	2026-02-25 02:23:41.741Z	40.456° NE	2026-02-25 02:26:41.741Z	88.739° E	23.976°	2026-02-25 02:30:41.741Z	138.768° SSE

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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, 61121 on other resources

View CZ-6A DEB, 61121 on Heavens-Above

View CZ-6A DEB, 61121 on Keep Track

View CZ-6A DEB, 61121 on Celestrak

View CZ-6A DEB, 61121 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, 61121

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 20 hours ago

TLE from 20 hours ago

TLE epoch observation values (Epoch: 2026-02-23T08:05:23.000Z)

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, 61121 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 20 hours ago