FENGYUN 2G AKM, 40369

Orbit data source: Space-Track

FENGYUN 2G AKM, 40369 is space debris in GEO originally from a launch on Wed, 31 Dec 2014 UTC launched from the Xichang Space Center, China (XSC). 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/40369?theme=dark&initialShowStats=false

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Identifier

40369, 2014-090C

Orbit

GEO

Country

CN / PRC

Related business

China Aerospace Science and Technology Corporation (CASC) (CN)

Manufacturer

China ARMT

Mission

Spacecraft

Bus & Motor

SHANXI AKM, Unknown motor

Mass

~50 kg wet, ~50 kg dry

Launch date (UTC)

2014-12-31 (11 years ago)

Launch vehicle

Unknown

Launch site

Xichang Space Center, China (XSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl + Cone, 0.8 m

Radar Cross Section

1.571 m², Medium (>0.1 m² and < 1m²)

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Last TLE update: 3 days ago

TLE from 3 days ago

0 FENGYUN 2G AKM
1 40369U 14090C   26170.85509479  .00000091  00000-0  00000+0 0  9998
2 40369   7.5633  68.5803 0046611 172.3847 187.5632  0.99586975 41665

Epoch: 2026-06-19T20:31Z

TLE epoch observation values (Epoch: 2026-06-19T20:31:20.189Z)

Latitude

0.00001°

Longitude

-147.43652°

Altitude

36,175.401 km

Speed

3.054 km/s

True Right ascension

04h 33m 54s

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

21:39:55

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

36,178.149 km

Perigee altitude

35,783.271 km

Semi-major axis

42,358.847 km

Eccentricity

0.00466

Inclination

7.5633°

RAAN

68.5803°

Arg. of periapsis

172.3847°

True anomaly

187.4933°

Mean anomaly

187.5632°

Eccentric anomaly

187.52821°

Mean motion

0.24896 °/min

Orbital period

1,446.02 mins

BSTAR

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Computing Atmospheric mass density...

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Other satellites on launch #90 in the year 2014 (2014-12-31 UTC)

FENGYUN 2G DEB, 43646

CZ-3A R/B, 40368

FENGYUN 2G, 40367

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FENGYUN 2G AKM 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.
1440 mins	2026-06-22 10:37:52.693Z	237.753° WSW	2026-06-23 02:59:52.693Z	248.642° W	24.171°	2026-06-23 10:37:52.693Z	239.963° WSW

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40369 neighbors

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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 FENGYUN 2G AKM, 40369 on other resources

View FENGYUN 2G AKM, 40369 on Heavens-Above

View FENGYUN 2G AKM, 40369 on Keep Track

View FENGYUN 2G AKM, 40369 on Celestrak

View FENGYUN 2G AKM, 40369 on Gunter's Space Page

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

FENGYUN 2G AKM, 40369

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: 2026-06-19T20:31:20.189Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #90 in the year 2014 (2014-12-31 UTC)

FENGYUN 2G AKM Visibility forecast

40369 neighbors

Co-orbital & Co-planar RSOs

Check out FENGYUN 2G AKM, 40369 on other resources

Documentation

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