YAOGAN 1 DEB, 36365

Orbit data source: Space-Track

YAOGAN 1 DEB, 36365 is space debris in SSO originally from a launch on Wed, 26 Apr 2006 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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Iframe URL

https://www.satcat.com/sats-embedded/36365?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

36365, 2006-015J

Orbit

SSO

Last TLE update

10 hours ago

Origin

China National Space Administration (CN / PRC)

Manufacturer

SAST

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

2006-04-26 (19 years ago)

Launch vehicle

Unknown

Launch site

Taiyaun Space Center, China (TSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown

Radar Cross Section

Large (>1 m²)

Expand to show TLE details & history

TLE from 10 hours ago

0 YAOGAN 1 DEB
1 36365U 06015J   25214.15299464  .00009665  00000-0  58803-3 0  9992
2 36365  97.8142 273.8942 0014134 202.3058 157.7557 15.10566870840080

Epoch: 2025-08-02T03:40Z

TLE epoch observation values (Epoch: 2025-08-02T03:40:18.736Z)

Latitude

-0.00013°

Longitude

-92.17711°

Altitude

546.583 km

Speed

7.584 km/s

True Right ascension

18h 15m 34s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

Latitude

10.76251°

Longitude

89.7468°

Altitude

528.44 km

Speed

7.604 km/s

Apparent Right ascension

09h 27m 36s

Apparent Declination

-32° 27' 12"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

03:42:38

Azimuth

117.966° SE

Elevation

-17.572°

Doppler factor

Orbital elements

Apogee altitude

541.232 km

Perigee altitude

521.7 km

Semi-major axis

6,909.603 km

Eccentricity

0.00141

Inclination

97.8142°

RAAN

273.8942°

Arg. of periapsis

202.3058°

True anomaly

157.81691°

Mean anomaly

157.7557°

Eccentric anomaly

157.78632°

Mean motion

3.77888 °/min

Orbital period

95.27 mins

BSTAR

0.00058803

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Other satellites on launch #15 in the year 2006 (2006-04-26 UTC)

YAOGAN 1, 29092

CZ-4B R/B, 29093 (Decayed)

YAOGAN 1 DEB, 36363 (Decayed)

YAOGAN 1 DEB, 36364 (Decayed)

YAOGAN 1 DEB, 36502 (Decayed)

YAOGAN 1 DEB, 36503 (Decayed)

YAOGAN 1 DEB, 36504 (Decayed)

YAOGAN 1 DEB, 37243 (Decayed)

YAOGAN 1 DEB Visibility forecast

Observer location: undefined°, undefined°

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	2025-08-02 16:57:26.873Z	10.995° NNE	2025-08-02 17:00:26.873Z	263.276° W	44.887°	2025-08-02 17:03:26.873Z	195.589° SSW
6 mins	2025-08-03 03:39:26.873Z	139.458° SSE	2025-08-03 03:42:26.873Z	58.178° ENE	34.353°	2025-08-03 03:45:26.873Z	2.851° NNE

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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Authenticating...

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Check out YAOGAN 1 DEB, 36365 on other resources

View YAOGAN 1 DEB, 36365 on Heavens-Above

View YAOGAN 1 DEB, 36365 on Keep Track

View YAOGAN 1 DEB, 36365 on Celestrak

View YAOGAN 1 DEB, 36365 on Gunter's Space Page

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