CZ-6A DEB, 61482

Orbit data source: Space-Track

CZ-6A DEB, 61482 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/61482?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

61482, 2024-140AAQ

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: 14 hours ago

TLE from 14 hours ago

0 CZ-6A DEB
1 61482U 24140AAQ 26054.59823426  .00003097  00000-0  60435-3 0  9998
2 61482  89.0614 288.0455 0107528 284.8644  74.0678 14.59100120 78169

Epoch: 2026-02-23T14:21Z

TLE epoch observation values (Epoch: 2026-02-23T14:21:27.440Z)

Latitude

-0.00002°

Longitude

-80.80865°

Altitude

679.065 km

Speed

7.528 km/s

True Right ascension

19h 12m 10s

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

07:21:54

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

769.01 km

Perigee altitude

616.941 km

Semi-major axis

7,071.113 km

Eccentricity

0.01075

Inclination

89.0614°

RAAN

288.0455°

Arg. of periapsis

284.8644°

True anomaly

75.25695°

Mean anomaly

74.0678°

Eccentric anomaly

74.66195°

Mean motion

3.65016 °/min

Orbital period

98.63 mins

BSTAR

0.00060435

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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.
9 mins	2026-02-24 04:06:10.010Z	351.741° N	2026-02-24 04:10:10.010Z	287.363° WNW	40.981°	2026-02-24 04:15:10.010Z	195.899° SSW
7 mins	2026-02-24 15:11:10.010Z	131.846° SE	2026-02-24 15:14:10.010Z	75.916° E	28.303°	2026-02-24 15:18:10.010Z	19.833° NNE
6 mins	2026-02-24 16:50:10.010Z	236.594° WSW	2026-02-24 16:53:10.010Z	287.446° WNW	22.613°	2026-02-24 16:56:10.010Z	328.288° NNW
7 mins	2026-02-25 03:10:10.010Z	29.565° NE	2026-02-25 03:13:10.010Z	91.44° ESE	32.404°	2026-02-25 03:17:10.010Z	152.601° 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, 61482 on other resources

View CZ-6A DEB, 61482 on Heavens-Above

View CZ-6A DEB, 61482 on Keep Track

View CZ-6A DEB, 61482 on Celestrak

View CZ-6A DEB, 61482 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, 61482

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: 2026-02-23T14:21:27.440Z)

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, 61482 on other resources

Documentation

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