SJ 16-02 DEB, 43429

Orbit data source: Space-Track

SJ 16-02 DEB, 43429 is space debris in LEO originally from a launch on Wed, 29 Jun 2016 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/43429?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

43429, 2016-043D

Orbit

LEO

Country

CN / PRC

Related business

China National Space Administration (CN)

Manufacturer

SAST

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

2016-06-29 (10 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: 3 days ago

TLE from 3 days ago

0 SJ 16-02 DEB
1 43429U 16043D   26170.33260593  .00001591  00000-0  31399-3 0  9997
2 43429  74.9638  44.4589 0193667 314.7725  43.7822 14.51918321521713

Epoch: 2026-06-19T07:58Z

TLE epoch observation values (Epoch: 2026-06-19T07:58:57.152Z)

Latitude

-0.00001°

Longitude

17.15767°

Altitude

624.119 km

Speed

7.599 km/s

True Right ascension

02h 57m 50s

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

23:09:18

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

854.325 km

Perigee altitude

579.51 km

Semi-major axis

7,095.054 km

Eccentricity

0.01937

Inclination

74.9638°

RAAN

44.4589°

Arg. of periapsis

314.7725°

True anomaly

45.34485°

Mean anomaly

43.7822°

Eccentric anomaly

44.56079°

Mean motion

3.6317 °/min

Orbital period

99.13 mins

BSTAR

0.00031399

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Other satellites on launch #43 in the year 2016 (2016-06-29 UTC)

CZ-4B R/B, 41635 (Decayed)

SJ 16-02, 41634

SJ 16-02 DEB, 43428

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SJ 16-02 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.
7 mins	2026-06-22 15:29:01.354Z	150.006° SSE	2026-06-22 15:32:01.354Z	104.192° ESE	25.254°	2026-06-22 15:36:01.354Z	43.82° NE
7 mins	2026-06-22 17:10:01.354Z	243.945° WSW	2026-06-22 17:13:01.354Z	294.433° NW	27.039°	2026-06-22 17:17:01.354Z	354.139° N
9 mins	2026-06-23 01:51:01.354Z	3.831° NNE	2026-06-23 01:55:01.354Z	71.48° E	33.727°	2026-06-23 02:00:01.354Z	136.305° SSE
8 mins	2026-06-23 03:32:01.354Z	309.819° NW	2026-06-23 03:35:01.354Z	271.586° WNW	23.754°	2026-06-23 03:40:01.354Z	208.878° SW

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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 SJ 16-02 DEB, 43429 on other resources

View SJ 16-02 DEB, 43429 on Heavens-Above

View SJ 16-02 DEB, 43429 on Keep Track

View SJ 16-02 DEB, 43429 on Celestrak

View SJ 16-02 DEB, 43429 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

SJ 16-02 DEB, 43429

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 3 days ago

TLE from 3 days ago

TLE epoch observation values (Epoch: 2026-06-19T07:58:57.152Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #43 in the year 2016 (2016-06-29 UTC)

SJ 16-02 DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out SJ 16-02 DEB, 43429 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 3 days ago