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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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 (14 years ago)

Launch vehicle

Unknown

Launch site

Jiuquan Satellite Launch Center, China (JSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 0.050 m

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 13 hours ago

TLE from 13 hours ago

0 CZ-2D DEB
1 43402U 12052B   26306.19826853  .00001002  00000-0  26163-3 0  9996
2 43402  98.0814  35.3402 0202059 348.3035  11.3497 14.40116503674632

Epoch: 2026-11-02T04:45Z

TLE epoch observation values (Epoch: 2026-11-02T04:45:30.400Z)

Latitude

-0.00001°

Longitude

-77.51519°

Altitude

619.79 km

Speed

7.623 km/s

True Right ascension

02h 21m 21s

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

13:36:21

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

899.35 km

Perigee altitude

611.078 km

Semi-major axis

7,133.351 km

Eccentricity

0.02021

Inclination

98.0814°

RAAN

35.3402°

Arg. of periapsis

348.3035°

True anomaly

11.81692°

Mean anomaly

11.3497°

Eccentric anomaly

11.58214°

Mean motion

3.60249 °/min

Orbital period

99.93 mins

BSTAR

0.00026163

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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.
10 mins	2026-11-02 18:39:46.477Z	20.729° NNE	2026-11-02 18:44:46.477Z	102.416° ESE	63.478°	2026-11-02 18:49:46.477Z	180.683° SSW
6 mins	2026-11-02 20:20:46.477Z	325.96° NNW	2026-11-02 20:22:46.477Z	300.824° NW	19.344°	2026-11-02 20:26:46.477Z	254.744° W
7 mins	2026-11-03 05:54:46.477Z	151.056° SSE	2026-11-03 05:56:46.477Z	110.135° ESE	64.112°	2026-11-03 06:01:46.477Z	352.539° 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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Check out CZ-2D DEB, 43402 on other resources

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View CZ-2D DEB, 43402 on Celestrak

View CZ-2D DEB, 43402 on Gunter's Space Page

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CZ-2D DEB, 43402

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 13 hours ago

TLE from 13 hours ago

TLE epoch observation values (Epoch: 2026-11-02T04:45:30.400Z)

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: 13 hours ago