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: 23 hours ago

TLE from 23 hours ago

0 YAOGAN 29 DEB
1 42673U 15069F   26132.36570627  .00000656  00000-0  71893-4 0  9992
2 42673  97.8784 168.2035 0004629 117.5775 242.5914 14.91113158566644

Epoch: 2026-05-12T08:46Z

TLE epoch observation values (Epoch: 2026-05-12T08:46:37.021Z)

Latitude

-0.00001°

Longitude

166.40813°

Altitude

598.988 km

Speed

7.559 km/s

True Right ascension

11h 12m 48s

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

16:33:48

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

594.715 km

Perigee altitude

588.262 km

Semi-major axis

6,969.625 km

Eccentricity

0.00046

Inclination

97.8784°

RAAN

168.2035°

Arg. of periapsis

117.5775°

True anomaly

242.54432°

Mean anomaly

242.5914°

Eccentric anomaly

242.56786°

Mean motion

3.73017 °/min

Orbital period

96.51 mins

BSTAR

0.000071893

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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.
6 mins	2026-05-13 14:20:52.670Z	47.026° ENE	2026-05-13 14:23:52.670Z	94.989° ESE	19.146°	2026-05-13 14:26:52.670Z	142.374° SSE
6 mins	2026-05-13 15:56:52.670Z	342.134° N	2026-05-13 15:59:52.670Z	277.776° WNW	26.388°	2026-05-13 16:02:52.670Z	229.734° WSW
6 mins	2026-05-14 02:46:52.670Z	193.248° SSW	2026-05-14 02:49:52.670Z	273.551° WNW	35.736°	2026-05-14 02:52:52.670Z	331.536° 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 YAOGAN 29 DEB, 42673 on other resources

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View YAOGAN 29 DEB, 42673 on Gunter's Space Page

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YAOGAN 29 DEB, 42673

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 23 hours ago

TLE from 23 hours ago

TLE epoch observation values (Epoch: 2026-05-12T08:46:37.021Z)

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: 23 hours ago