FENGYUN 1C DEB, 41822

Orbit data source: Space-Track

FENGYUN 1C DEB, 41822 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.

Loading next visibility...

Iframe embed code

<iframe src="https://www.satcat.com/sats-embedded/41822?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

Iframe URL

https://www.satcat.com/sats-embedded/41822?theme=dark&initialShowStats=false

Optional Secondary NORAD IDs

Max 10 NORAD IDs; Separated by commas

Initial load time (optional)

ISO8601 Format

TLE date request (optional)

ISO8601 Format

Identifier

41822, 1999-025EXZ

Orbit

SSO

Last TLE update

20 hours 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 20 hours ago

0 FENGYUN 1C DEB
1 41822U 99025EXZ 25199.14319817  .00001908  00000-0  84533-3 0  9996
2 41822  98.7429 266.2299 0053492 288.8638  70.6744 14.23543886452722

Epoch: 2025-07-18T03:26Z

TLE epoch observation values (Epoch: 2025-07-18T03:26:12.321Z)

Latitude

-0.0001°

Longitude

-81.52031°

Altitude

803.761 km

Speed

7.458 km/s

True Right ascension

17h 44m 55s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

Latitude

-23.07159°

Longitude

-76.95088°

Altitude

797.39 km

Speed

7.467 km/s

Apparent Right ascension

20h 35m 58s

Apparent Declination

-41° 00' 52"

Sunlit

Object is in full shadow

Visualization observer readout

Local Sidereal Time

12:21:53

Azimuth

110.561° ESE

Elevation

-47.791°

Doppler factor

Orbital elements

Apogee altitude

849.002 km

Perigee altitude

772.094 km

Semi-major axis

7,188.685 km

Eccentricity

0.00535

Inclination

98.7429°

RAAN

266.2299°

Arg. of periapsis

288.8638°

True anomaly

71.25411°

Mean anomaly

70.6744°

Eccentric anomaly

70.96413°

Mean motion

3.56098 °/min

Orbital period

101.1 mins

BSTAR

0.00084533

Loading maneuver chart data...

Loading SW <> Apogee altitude chart data...

Loading historical data...

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, 30314

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.
7 mins	2025-07-19 03:12:15.520Z	107.76° ESE	2025-07-19 03:16:15.520Z	58.832° ENE	18.941°	2025-07-19 03:19:15.520Z	22.121° NNE
8 mins	2025-07-19 04:52:15.520Z	190.508° SSW	2025-07-19 04:55:15.520Z	250.124° W	38.944°	2025-07-19 05:00:15.520Z	335.575° NNW
9 mins	2025-07-19 17:08:15.520Z	22.896° NE	2025-07-19 17:12:15.520Z	83.639° E	41.472°	2025-07-19 17:17:15.520Z	181.423° SSW
5 mins	2025-07-19 18:50:15.520Z	320.382° NNW	2025-07-19 18:52:15.520Z	293.781° NW	17.146°	2025-07-19 18:55:15.520Z	259.141° W

Co-orbital & Co-planar RSOs

Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions

Click to sort rows by RSO header in ascending order	Click to sort rows by Country header in ascending order	Click to sort rows by Type header in ascending order	Click to sort rows by Inclination Δ header in ascending order	Click to sort rows by RAAN Δ header in ascending order	Click to sort rows by Coplanar Angle header in ascending order	Click to sort rows by SMA Δ header in ascending order	Click to sort rows by Orbital period header in ascending order	Click to sort rows by <5km Md TCA header in ascending order

Authenticating...

Click to sort rows by Secondary header in ascending order	Click to sort rows by Secondary name header in ascending order	Click to sort rows by Country header in ascending order	Click to sort rows by Owner header in ascending order	Click to sort rows by Obj. Type header in ascending order	Click to sort rows by Miss dist. header in ascending order	Click to sort rows by Rel. speed header in ascending order	Click to sort rows by Apr. angle header in ascending order	Click to sort rows by TCA header in ascending order

Check out FENGYUN 1C DEB, 41822 on other resources

View FENGYUN 1C DEB, 41822 on Heavens-Above

View FENGYUN 1C DEB, 41822 on Keep Track

View FENGYUN 1C DEB, 41822 on Celestrak

View FENGYUN 1C DEB, 41822 on Gunter's Space Page

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