CZ-6A DEB, 60628

Orbit data source: Space-Track

CZ-6A DEB, 60628 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/60628?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

60628, 2024-140AD

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, 0.3 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago

0 CZ-6A DEB
1 60628U 24140AD  26114.44917242  .00000470  00000-0  17771-3 0  9997
2 60628  88.8316 267.3612 0007120  66.5621 293.6322 14.29582386 89193

Epoch: 2026-04-24T10:46Z

TLE epoch observation values (Epoch: 2026-04-24T10:46:48.497Z)

Latitude

-0.00002°

Longitude

-106.82261°

Altitude

794.149 km

Speed

7.458 km/s

True Right ascension

17h 49m 26s

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

05:45:35

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

795.169 km

Perigee altitude

784.962 km

Semi-major axis

7,168.203 km

Eccentricity

0.00071

Inclination

88.8316°

RAAN

267.3612°

Arg. of periapsis

66.5621°

True anomaly

293.55743°

Mean anomaly

293.6322°

Eccentric anomaly

293.59482°

Mean motion

3.57625 °/min

Orbital period

100.66 mins

BSTAR

0.00017771

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

CZ-6A DEB, 60629 (Decayed)

CZ-6A DEB, 61392 (Decayed)

CZ-6A DEB, 60851 (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	2026-04-24 23:07:11.716Z	341.622° N	2026-04-24 23:11:11.716Z	281.759° WNW	32.292°	2026-04-24 23:15:11.716Z	215.158° SW
9 mins	2026-04-25 10:25:11.716Z	168.192° S	2026-04-25 10:29:11.716Z	74.193° E	43.554°	2026-04-25 10:34:11.716Z	3.699° NNE

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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, 60628 on other resources

View CZ-6A DEB, 60628 on Heavens-Above

View CZ-6A DEB, 60628 on Keep Track

View CZ-6A DEB, 60628 on Celestrak

View CZ-6A DEB, 60628 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, 60628

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 12 hours ago

TLE from 12 hours ago

TLE epoch observation values (Epoch: 2026-04-24T10:46:48.497Z)

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, 60628 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 12 hours ago