CZ-6A DEB, 60630

Orbit data source: Space-Track

CZ-6A DEB, 60630 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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https://www.satcat.com/sats-embedded/60630?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

60630, 2024-140AF

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, 0.2 m

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 17 hours ago

TLE from 17 hours ago

0 CZ-6A DEB
1 60630U 24140AF  26053.91164824  .00086048  00000-0  54184-2 0  9997
2 60630  88.2887 229.9408 0091680 148.2031 212.4789 15.05331978 83056

Epoch: 2026-02-22T21:52Z

TLE epoch observation values (Epoch: 2026-02-22T21:52:46.407Z)

Latitude

-0.00003°

Longitude

108.93435°

Altitude

607.423 km

Speed

7.526 km/s

True Right ascension

15h 19m 45s

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

18:29:44

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

610.815 km

Perigee altitude

483.829 km

Semi-major axis

6,925.459 km

Eccentricity

0.00917

Inclination

88.2887°

RAAN

229.9408°

Arg. of periapsis

148.2031°

True anomaly

211.92017°

Mean anomaly

212.4789°

Eccentric anomaly

212.19899°

Mean motion

3.76591 °/min

Orbital period

95.59 mins

BSTAR

0.0054184

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

QIANFAN-8, 60386

CZ-6A DEB, 61343 (Decayed)

CZ-6A DEB, 61342 (Decayed)

CZ-6A DEB, 61495 (Decayed)

CZ-6A DEB, 61844 (Decayed)

CZ-6A DEB, 60851 (Decayed)

CZ-6A DEB, 61457 (Decayed)

CZ-6A DEB, 61407 (Decayed)

CZ-6A DEB, 61284 (Decayed)

CZ-6A DEB, 60888 (Decayed)

CZ-6A DEB, 61496 (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	2026-02-23 23:58:06.810Z	357.701° N	2026-02-24 00:01:06.810Z	327.21° NNW	43.887°	2026-02-24 00:04:06.810Z	185.057° SSW
6 mins	2026-02-24 12:18:06.810Z	196.257° SSW	2026-02-24 12:21:06.810Z	302.502° NW	39.679°	2026-02-24 12:24:06.810Z	350.679° N

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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, 60630 on other resources

View CZ-6A DEB, 60630 on Heavens-Above

View CZ-6A DEB, 60630 on Keep Track

View CZ-6A DEB, 60630 on Celestrak

View CZ-6A DEB, 60630 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, 60630

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 17 hours ago

TLE from 17 hours ago

TLE epoch observation values (Epoch: 2026-02-22T21:52:46.407Z)

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, 60630 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 17 hours ago