CZ-6A DEB, 61100

Orbit data source: Space-Track

CZ-6A DEB, 61100 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/61100?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

61100, 2024-140NS

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: 4 hours ago

TLE from 4 hours ago

0 CZ-6A DEB
1 61100U 24140NS  26117.19345568  .00001571  00000-0  32360-3 0  9998
2 61100  89.0327 279.2491 0114666  79.5272 281.8835 14.55863607 88195

Epoch: 2026-04-27T04:38Z

TLE epoch observation values (Epoch: 2026-04-27T04:38:34.570Z)

Latitude

-0.00001°

Longitude

-5.58157°

Altitude

693.83 km

Speed

7.518 km/s

True Right ascension

18h 36m 59s

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

16:09:46

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

784.663 km

Perigee altitude

622.259 km

Semi-major axis

7,081.598 km

Eccentricity

0.01147

Inclination

89.0327°

RAAN

279.2491°

Arg. of periapsis

79.5272°

True anomaly

280.59399°

Mean anomaly

281.8835°

Eccentric anomaly

281.23911°

Mean motion

3.64205 °/min

Orbital period

98.85 mins

BSTAR

0.0003236

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

CZ-6A DEB, 60806 (Decayed)

CZ-6A DEB, 61289 (Decayed)

CZ-6A DEB, 60677 (Decayed)

CZ-6A DEB, 61343 (Decayed)

CZ-6A DEB, 61377 (Decayed)

CZ-6A DEB, 60647 (Decayed)

CZ-6A DEB, 60638 (Decayed)

CZ-6A DEB, 61427 (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	2026-04-27 11:20:49.004Z	182.949° SSW	2026-04-27 11:24:49.004Z	215.429° SW	42.785°	2026-04-27 11:28:49.004Z	354.554° N
7 mins	2026-04-27 23:21:49.004Z	350.253° N	2026-04-27 23:24:49.004Z	291.808° WNW	41.048°	2026-04-27 23:28:49.004Z	196.286° 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, 61100 on other resources

View CZ-6A DEB, 61100 on Heavens-Above

View CZ-6A DEB, 61100 on Keep Track

View CZ-6A DEB, 61100 on Celestrak

View CZ-6A DEB, 61100 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, 61100

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 4 hours ago

TLE from 4 hours ago

TLE epoch observation values (Epoch: 2026-04-27T04:38:34.570Z)

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, 61100 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 4 hours ago