YAOGAN 30 DEB, 42676

Orbit data source: Space-Track

YAOGAN 30 DEB, 42676 is space debris in SSO originally from a launch on Sun, 15 May 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/42676?theme=dark&initialShowStats=false

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Identifier

42676, 2016-029B

Orbit

SSO

Country

CN / PRC

Related business

China National Space Administration (CN)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

2016-05-15 (10 years ago)

Launch vehicle

Unknown

Launch site

Jiuquan Satellite Launch Center, China (JSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 0.050 m

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 16 hours ago

TLE from 16 hours ago

0 YAOGAN 30 DEB
1 42676U 16029B   26297.26612991  .00001014  00000-0  29347-3 0  9999
2 42676  98.0450 114.6938 0231834  69.0804 293.5027 14.31907331530539

Epoch: 2026-10-24T06:23Z

TLE epoch observation values (Epoch: 2026-10-24T06:23:13.624Z)

Latitude

-0.00005°

Longitude

-13.78775°

Altitude

725.355 km

Speed

7.525 km/s

True Right ascension

07h 38m 46s

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

17:26:00

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

948.479 km

Perigee altitude

616.465 km

Semi-major axis

7,160.609 km

Eccentricity

0.02318

Inclination

98.045°

RAAN

114.6938°

Arg. of periapsis

69.0804°

True anomaly

291.03876°

Mean anomaly

293.5027°

Eccentric anomaly

292.2735°

Mean motion

3.58194 °/min

Orbital period

100.5 mins

BSTAR

0.00029347

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Other satellites on launch #29 in the year 2016 (2016-05-15 UTC)

YAOGAN 30 DEB, 42677

YAOGAN 30, 41473

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YAOGAN 30 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.
6 mins	2026-10-24 23:45:10.671Z	57.835° ENE	2026-10-24 23:48:10.671Z	102.281° ESE	19.146°	2026-10-24 23:51:10.671Z	139.073° SSE
7 mins	2026-10-25 01:24:10.671Z	350.642° N	2026-10-25 01:27:10.671Z	290.751° WNW	43.255°	2026-10-25 01:31:10.671Z	221.118° SW
5 mins	2026-10-25 11:03:10.671Z	108.797° ESE	2026-10-25 11:05:10.671Z	75.57° E	22.363°	2026-10-25 11:08:10.671Z	23.571° NE
6 mins	2026-10-25 12:42:10.671Z	211.795° SW	2026-10-25 12:45:10.671Z	270.336° WNW	28.913°	2026-10-25 12:48:10.671Z	320.338° 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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Check out YAOGAN 30 DEB, 42676 on other resources

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View YAOGAN 30 DEB, 42676 on Celestrak

View YAOGAN 30 DEB, 42676 on Gunter's Space Page

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YAOGAN 30 DEB, 42676

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 16 hours ago

TLE from 16 hours ago

TLE epoch observation values (Epoch: 2026-10-24T06:23:13.624Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #29 in the year 2016 (2016-05-15 UTC)

YAOGAN 30 DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out YAOGAN 30 DEB, 42676 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 16 hours ago