CZ-6A DEB, 61157

Orbit data source: Space-Track

CZ-6A DEB, 61157 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/61157?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

61157, 2024-140RB

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

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 14 hours ago

TLE from 14 hours ago

0 CZ-6A DEB
1 61157U 24140RB  26171.26888653  .00000698  00000-0  24504-3 0  9995
2 61157  88.8508 260.7752 0095137  51.4777 309.4900 14.31365435 95390

Epoch: 2026-06-20T06:27Z

TLE epoch observation values (Epoch: 2026-06-20T06:27:11.796Z)

Latitude

-0.00002°

Longitude

-104.50989°

Altitude

747.268 km

Speed

7.503 km/s

True Right ascension

17h 23m 06s

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

07:18:15

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

852.245 km

Perigee altitude

715.966 km

Semi-major axis

7,162.243 km

Eccentricity

0.00951

Inclination

88.8508°

RAAN

260.7752°

Arg. of periapsis

51.4777°

True anomaly

308.64228°

Mean anomaly

309.49°

Eccentric anomaly

309.06678°

Mean motion

3.58071 °/min

Orbital period

100.54 mins

BSTAR

0.00024504

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

CZ-6A DEB, 60882

CZ-6A DEB, 61384 (Decayed)

CZ-6A DEB, 60744 (Decayed)

CZ-6A DEB, 60849

CZ-6A DEB, 60885

CZ-6A DEB, 61344 (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.
8 mins	2026-06-21 06:03:29.564Z	159.211° S	2026-06-21 06:07:29.564Z	87.816° E	38.943°	2026-06-21 06:11:29.564Z	11.363° NNE
8 mins	2026-06-21 18:16:29.564Z	0.471° NNE	2026-06-21 18:19:29.564Z	354.871° N	44.53°	2026-06-21 18:24:29.564Z	182.827° SSW

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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, 61157 on other resources

View CZ-6A DEB, 61157 on Heavens-Above

View CZ-6A DEB, 61157 on Keep Track

View CZ-6A DEB, 61157 on Celestrak

View CZ-6A DEB, 61157 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, 61157

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 14 hours ago

TLE from 14 hours ago

TLE epoch observation values (Epoch: 2026-06-20T06:27:11.796Z)

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, 61157 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 14 hours ago