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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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, 0.1 m

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago

0 CZ-2D DEB
1 43402U 12052B   26094.72076198  .00003774  00000-0  96510-3 0  9999
2 43402  98.0766 195.6270 0203456 268.6844  89.1031 14.39322308644202

Epoch: 2026-04-04T17:17Z

TLE epoch observation values (Epoch: 2026-04-04T17:17:53.835Z)

Latitude

-0.00004°

Longitude

103.11621°

Altitude

764.382 km

Speed

7.472 km/s

True Right ascension

13h 02m 30s

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

23:15:04

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

903.026 km

Perigee altitude

612.654 km

Semi-major axis

7,135.977 km

Eccentricity

0.02035

Inclination

98.0766°

RAAN

195.627°

Arg. of periapsis

268.6844°

True anomaly

91.43453°

Mean anomaly

89.1031°

Eccentric anomaly

90.2688°

Mean motion

3.6005 °/min

Orbital period

99.99 mins

BSTAR

0.0009651

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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.
9 mins	2026-04-05 18:55:27.705Z	31.52° NE	2026-04-05 18:59:27.705Z	87.465° E	32.921°	2026-04-05 19:04:27.705Z	165.209° S
7 mins	2026-04-05 20:35:27.705Z	337.543° N	2026-04-05 20:38:27.705Z	294.14° NW	24.378°	2026-04-05 20:42:27.705Z	241.584° WSW
9 mins	2026-04-06 06:08:27.705Z	136.821° SSE	2026-04-06 06:12:27.705Z	58.513° ENE	36.462°	2026-04-06 06:17:27.705Z	358.829° N
7 mins	2026-04-06 07:48:27.705Z	229.807° WSW	2026-04-06 07:51:27.705Z	271.575° WNW	21.041°	2026-04-06 07:55:27.705Z	317.747° NNW

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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-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: 1 day ago

TLE from 1 day ago

TLE epoch observation values (Epoch: 2026-04-04T17:17:53.835Z)

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: 1 day ago