FENGYUN 1C DEB *

Satellite information

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Satellite Type and Status

DEBRISIN ORBIT

Key statistics

Satellite FENGYUN 1C DEB * at a glance.

Uptime

9611

Days in orbit

Revolutions

≈ 14.4

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

99.0

Latest

Satellite identification and parameters

Extended collection of information and parameters for FENGYUN 1C DEB *.

Object identification

Identified? True

Debris? True

Object name: FENGYUN 1C DEB *

International designator: 1999-025FBB

Object number (NORAD): 47025

Object ID (CCSDS): 47025

Country: PEOPLES REPUBLIC OF CHINA (PRC)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 99.707 minutes

Inclination: 99.0437 deg

SMA: 7122.71 km

Apoapsis: 773.487 km

Periapsis: 715.663 km

RAAN: 82.3771 deg

Eccentricy: 0.00405916

Argument of periapsis: 309.7189 deg

Mean anomaly: 80.3083 deg

Mean motion: 14.44225006 rev/day

Mean motion (dot): 0.00008669 rev/day2

B* drag term: 0.0025109708 1/REarth

Two-line elements (TLE)

Creation date: Aug. 31, 2025, 2:26 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Aug. 30, 2025, 12:08 p.m. UTC

TLE line 0: 0 FENGYUN 1C DEB *

TLE line 1: 1 47025U 99025FBB 25242.50582459 .00008669 00000-0 25110-2 0 9996

TLE line 2: 2 47025 99.0437 82.3771 0040592 309.7189 80.3083 14.44225006612365

Live tracking on map

Real-time ground track for satellite FENGYUN 1C DEB *.

In-orbit conjunctions

A list of the most updated potential collisions computed for object FENGYUN 1C DEB *.

Target Orbit TCA Probability of collision Miss distance Type
SL-8 R/B LEO 2025-05-24 21:25:53 0.0001740194 630.0 (m) ROCKET BODY
IRIDIUM 920 LEO 2025-02-10 07:29:09 0.0009828628 203.0 (m) PAYLOAD
FEDSAT SSO 2024-11-25 00:05:34 0.0001477451 862.0 (m) PAYLOAD
SL-16 DEB LEO 2024-11-15 02:39:48 0.0001598799 169.0 (m) DEBRIS
SL-16 DEB LEO 2024-11-15 01:50:12 0.0001514968 835.0 (m) DEBRIS

Associated space launch

Chinese polar orbiting meteorological satellite

FENGYUN 1C DEB * was lifted into orbit during the mission ‘Long March 4B | Feng Yun 1C’, on board a Long March 4B space rocket.

The launch took place on May 10, 1999, 1:33 a.m. from Launch Complex 7.

For more information about the launch, click the button.

Launch to space Long March 4B | Feng Yun 1C
Long March 4B | Feng Yun 1C

Agency: N/A

Status: Launch Successful

Launch date: May 10, 1999, 1:33 a.m. UTC

Rocket: Long March 4B

Launch pad: Launch Complex 7

Location: Taiyuan Satellite Launch Center, People's Republic of China

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