FENGYUN 1C DEB, 30314

Orbit data source: Space-Track

FENGYUN 1C DEB, 30314 is space debris in SSO originally from a launch on Mon, 10 May 1999 UTC launched from the Taiyaun Space Center, China (TSC). Fengyun 1C debris stems from the Chinese weather satellite Fengyun-1C, which was intentionally destroyed by a Chinese anti-satellite missile in 2007. This event dramatically increased the amount of space debris, with thousands of trackable fragments posing hazards to satellites and human spaceflight. The Fengyun 1C debris cloud has become a focal point in discussions about space sustainability and the need for international regulations to prevent the creation of new debris.

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https://www.satcat.com/sats-embedded/30314?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

30314, 1999-025AAB

Orbit

SSO

Last TLE update

2 days ago

Origin

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

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1999-05-10 (26 years ago)

Launch vehicle

Unknown

Launch site

Taiyaun Space Center, China (TSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history

TLE from 2 days ago

0 FENGYUN 1C DEB
1 30314U 99025AAB 25197.83517508  .00000909  00000-0  58233-3 0  9999
2 30314  98.3825  40.8627 0145147  56.9030 304.5975 14.00522300940249

Epoch: 2025-07-16T20:02Z

TLE epoch observation values (Epoch: 2025-07-16T20:02:39.126Z)

Latitude

-0.00005°

Longitude

165.29004°

Altitude

836.007 km

Speed

7.465 km/s

True Right ascension

02h 43m 27s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

35.17547°

Longitude

161.33397°

Altitude

794.743 km

Speed

7.512 km/s

Apparent Right ascension

01h 32m 37s

Apparent Declination

0° 13' 29"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

12:26:25

Azimuth

335.261° NNW

Elevation

-47.113°

Doppler factor

Orbital elements

Apogee altitude

994.638 km

Perigee altitude

783.673 km

Semi-major axis

7,267.293 km

Eccentricity

0.01451

Inclination

98.3825°

RAAN

40.8627°

Arg. of periapsis

56.903°

True anomaly

303.21426°

Mean anomaly

304.5975°

Eccentric anomaly

303.9073°

Mean motion

3.50336 °/min

Orbital period

102.76 mins

BSTAR

0.00058233

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Other satellites on launch #25 in the year 1999 (1999-05-10 UTC)

FENGYUN 1C, 25730

FENGYUN 1C DEB, 29736

FENGYUN 1C DEB, 30313

FENGYUN 1C DEB, 30315

FENGYUN 1C DEB, 30316

FENGYUN 1C DEB, 30317

FENGYUN 1C DEB, 30318 (Decayed)

FENGYUN 1C DEB, 30319 (Decayed)

FENGYUN 1C DEB, 30320

FENGYUN 1C DEB, 30321

FENGYUN 1C DEB, 30322

FENGYUN 1C DEB, 30325

FENGYUN 1C DEB, 30326

FENGYUN 1C DEB, 30327

FENGYUN 1C 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.
9 mins	2025-07-19 01:46:47.211Z	32.575° NE	2025-07-19 01:50:47.211Z	86.603° E	32.429°	2025-07-19 01:55:47.211Z	163.182° S
7 mins	2025-07-19 03:29:47.211Z	335.895° NNW	2025-07-19 03:32:47.211Z	290.333° WNW	25.03°	2025-07-19 03:36:47.211Z	240.565° WSW
8 mins	2025-07-19 13:19:47.211Z	153.873° SSE	2025-07-19 13:23:47.211Z	36.204° NE	42.269°	2025-07-19 13:27:47.211Z	352.605° N

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 FENGYUN 1C DEB, 30314 on other resources

View FENGYUN 1C DEB, 30314 on Heavens-Above

View FENGYUN 1C DEB, 30314 on Keep Track

View FENGYUN 1C DEB, 30314 on Celestrak

View FENGYUN 1C DEB, 30314 on Gunter's Space Page

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