CZ-2D DEB, 43402

Orbit data source: Space-Track

CZ-2D DEB, 43402 is space debris in SSO originally from a launch on Sat, 29 Sep 2012 UTC launched from the Jiuquan Satellite Launch Center, China (JSC). 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/43402?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

43402, 2012-052B

Orbit

SSO

Country

CN / PRC

Related business

China National Space Administration (CN)

Manufacturer

SAST

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

2012-09-29 (13 years ago)

Launch vehicle

Unknown

Launch site

Jiuquan Satellite Launch Center, China (JSC)

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-2D DEB
1 43402U 12052B   25292.74358620  .00004397  00000-0  11372-2 0  9997
2 43402  98.0802  38.2197 0208872  54.3546 307.6895 14.38093037620190

Epoch: 2025-10-19T17:50Z

TLE epoch observation values (Epoch: 2025-10-19T17:50:45.847Z)

Latitude

-0.00011°

Longitude

102.07282°

Altitude

678.521 km

Speed

7.564 km/s

True Right ascension

02h 32m 52s

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

02:40:38

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

911.045 km

Perigee altitude

612.774 km

Semi-major axis

7,140.046 km

Eccentricity

0.02089

Inclination

98.0802°

RAAN

38.2197°

Arg. of periapsis

54.3546°

True anomaly

305.7651°

Mean anomaly

307.6895°

Eccentric anomaly

306.73036°

Mean motion

3.59742 °/min

Orbital period

100.07 mins

BSTAR

0.0011372

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Other satellites on launch #52 in the year 2012 (2012-09-29 UTC)

CZ-2D DEB, 43403

VRSS-1, 38782

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CZ-2D 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	2025-10-20 19:28:00.257Z	33.974° NE	2025-10-20 19:32:00.257Z	110.719° ESE	32.818°	2025-10-20 19:36:00.257Z	166.523° S
6 mins	2025-10-20 21:08:00.257Z	330.292° NNW	2025-10-20 21:10:00.257Z	300.065° NW	20.649°	2025-10-20 21:14:00.257Z	245.136° WSW
6 mins	2025-10-21 06:44:00.257Z	130.8° SE	2025-10-21 06:46:00.257Z	76.359° E	35.235°	2025-10-21 06:50:00.257Z	0.829° NNE

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-2D DEB, 43402 on other resources

View CZ-2D DEB, 43402 on Heavens-Above

View CZ-2D DEB, 43402 on Keep Track

View CZ-2D DEB, 43402 on Celestrak

View CZ-2D DEB, 43402 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-2D DEB, 43402

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: 2025-10-19T17:50:45.847Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #52 in the year 2012 (2012-09-29 UTC)

CZ-2D DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out CZ-2D DEB, 43402 on other resources

Documentation

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