YAOGAN 29 DEB, 42673

Orbit data source: Space-Track

YAOGAN 29 DEB, 42673 is space debris in SSO originally from a launch on Thu, 26 Nov 2015 UTC launched from the Taiyaun Space Center, China (TSC). 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/42673?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

42673, 2015-069F

Orbit

SSO

Country

CN / PRC

Related business

China National Space Administration (CN)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

2015-11-26 (10 years ago)

Launch vehicle

Unknown

Launch site

Taiyaun Space Center, China (TSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 0.1 m

Radar Cross Section

Small (<0.1 m²)

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Last TLE update: 1 day ago

TLE from 1 day ago

0 YAOGAN 29 DEB
1 42673U 15069F   26123.37355519  .00001227  00000-0  12951-3 0  9998
2 42673  97.8795 159.2244 0004129 138.9373 221.2156 14.91097275565309

Epoch: 2026-05-03T08:57Z

TLE epoch observation values (Epoch: 2026-05-03T08:57:55.168Z)

Latitude

-0.00006°

Longitude

163.46651°

Altitude

599.717 km

Speed

7.559 km/s

True Right ascension

10h 36m 53s

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

00:40:54

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

594.416 km

Perigee altitude

588.66 km

Semi-major axis

6,969.675 km

Eccentricity

0.00041

Inclination

97.8795°

RAAN

159.2244°

Arg. of periapsis

138.9373°

True anomaly

221.18444°

Mean anomaly

221.2156°

Eccentric anomaly

221.20002°

Mean motion

3.73013 °/min

Orbital period

96.51 mins

BSTAR

0.00012951

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Other satellites on launch #69 in the year 2015 (2015-11-26 UTC)

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YAOGAN 29 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.
5 mins	2026-05-05 01:23:02.347Z	106.965° ESE	2026-05-05 01:25:02.347Z	75.924° E	17.719°	2026-05-05 01:28:02.347Z	26.158° NE
5 mins	2026-05-05 02:59:02.347Z	216.417° SW	2026-05-05 03:01:02.347Z	268.578° W	29.174°	2026-05-05 03:04:02.347Z	324.157° NNW
6 mins	2026-05-05 14:42:02.347Z	41.832° NE	2026-05-05 14:45:02.347Z	113.589° SE	28.841°	2026-05-05 14:48:02.347Z	162.192° S
4 mins	2026-05-05 16:18:02.347Z	324.998° NNW	2026-05-05 16:20:02.347Z	290.158° WNW	17.637°	2026-05-05 16:22:02.347Z	257.156° W

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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 29 DEB, 42673 on other resources

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View YAOGAN 29 DEB, 42673 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 29 DEB, 42673

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: 2026-05-03T08:57:55.168Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #69 in the year 2015 (2015-11-26 UTC)

YAOGAN 29 DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out YAOGAN 29 DEB, 42673 on other resources

Documentation

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