CZ-6A DEB, 61158

Orbit data source: Space-Track

CZ-6A DEB, 61158 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/61158?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

61158, 2024-140RC

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: 5 hours ago

TLE from 5 hours ago

0 CZ-6A DEB
1 61158U 24140RC  26118.80964159  .00002793  00000-0  11048-2 0  9999
2 61158  88.5003 242.5671 0082995 262.9395  96.2355 14.26864225 87569

Epoch: 2026-04-28T19:25Z

TLE epoch observation values (Epoch: 2026-04-28T19:25:53.033Z)

Latitude

-0.00002°

Longitude

94.31651°

Altitude

812.255 km

Speed

7.443 km/s

True Right ascension

16h 10m 16s

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

08:20:08

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

858.744 km

Perigee altitude

739.608 km

Semi-major axis

7,177.313 km

Eccentricity

0.0083

Inclination

88.5003°

RAAN

242.5671°

Arg. of periapsis

262.9395°

True anomaly

97.17982°

Mean anomaly

96.2355°

Eccentric anomaly

96.70777°

Mean motion

3.56944 °/min

Orbital period

100.86 mins

BSTAR

0.0011048

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

CZ-6A DEB, 61392 (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	2026-04-29 07:21:36.301Z	110.402° ESE	2026-04-29 07:24:36.301Z	75.945° E	16.029°	2026-04-29 07:27:36.301Z	41.266° NE
8 mins	2026-04-29 09:01:36.301Z	197.996° SSW	2026-04-29 09:04:36.301Z	249.689° W	40.64°	2026-04-29 09:09:36.301Z	350.215° N
8 mins	2026-04-29 19:35:36.301Z	30.254° NE	2026-04-29 19:39:36.301Z	89.079° E	25.453°	2026-04-29 19:43:36.301Z	139.429° SSE
8 mins	2026-04-29 21:16:36.301Z	333.61° NNW	2026-04-29 21:20:36.301Z	269.425° W	28.687°	2026-04-29 21:24:36.301Z	218.197° SW

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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, 61158 on other resources

View CZ-6A DEB, 61158 on Heavens-Above

View CZ-6A DEB, 61158 on Keep Track

View CZ-6A DEB, 61158 on Celestrak

View CZ-6A DEB, 61158 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, 61158

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 5 hours ago

TLE from 5 hours ago

TLE epoch observation values (Epoch: 2026-04-28T19:25:53.033Z)

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, 61158 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 5 hours ago