YAOGAN 30 DEB, 42677

Orbit data source: Space-Track

YAOGAN 30 DEB, 42677 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/42677?theme=dark&initialShowStats=false

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Identifier

42677, 2016-029C

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, 0.1 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 YAOGAN 30 DEB
1 42677U 16029C   26170.27907095  .00001042  00000-0  30290-3 0  9993
2 42677  98.0072 289.7792 0228972  51.0521 311.0827 14.31992781512175

Epoch: 2026-06-19T06:41Z

TLE epoch observation values (Epoch: 2026-06-19T06:41:51.730Z)

Latitude

-0.00003°

Longitude

-78.19667°

Altitude

682.408 km

Speed

7.571 km/s

True Right ascension

19h 19m 07s

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

21:29:38

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

946.137 km

Perigee altitude

618.234 km

Semi-major axis

7,160.322 km

Eccentricity

0.0229

Inclination

98.0072°

RAAN

289.7792°

Arg. of periapsis

51.0521°

True anomaly

309.0675°

Mean anomaly

311.0827°

Eccentric anomaly

310.07888°

Mean motion

3.58215 °/min

Orbital period

100.5 mins

BSTAR

0.0003029

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

YAOGAN 30, 41473

YAOGAN 30 DEB, 42676

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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.
9 mins	2026-06-22 20:46:37.599Z	14.887° NNE	2026-06-22 20:50:37.599Z	39.169° NE	43.762°	2026-06-22 20:55:37.599Z	190.454° SSW
6 mins	2026-06-23 08:05:37.599Z	174.494° S	2026-06-23 08:08:37.599Z	304.857° NW	43.195°	2026-06-23 08:11:37.599Z	342.731° 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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings

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Check out YAOGAN 30 DEB, 42677 on other resources

View YAOGAN 30 DEB, 42677 on Heavens-Above

View YAOGAN 30 DEB, 42677 on Keep Track

View YAOGAN 30 DEB, 42677 on Celestrak

View YAOGAN 30 DEB, 42677 on Gunter's Space Page

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

YAOGAN 30 DEB, 42677

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: 2026-06-19T06:41:51.730Z)

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, 42677 on other resources

Documentation

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