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

≈ 14.1

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

99.2

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: 1999-025VT

Object number (NORAD): 30210

Object ID (CCSDS): 30210

Country: PEOPLES REPUBLIC OF CHINA (PRC)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 102.275 minutes

Inclination: 99.2034 deg

SMA: 7244.452 km

Apoapsis: 907.671 km

Periapsis: 824.963 km

RAAN: 291.5236 deg

Eccentricy: 0.00570839

Argument of periapsis: 64.243 deg

Mean anomaly: 59.9261 deg

Mean motion: 14.07973493 rev/day

Mean motion (dot): 0.00001326 rev/day2

B* drag term: 0.00079541018 1/REarth

Two-line elements (TLE)

Creation date: Sept. 1, 2025, 2:20 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Aug. 31, 2025, 4:52 p.m. UTC

TLE line 0: 0 FENGYUN 1C DEB

TLE line 1: 1 30210U 99025VT 25243.70288159 .00001326 00000-0 79541-3 0 9998

TLE line 2: 2 30210 99.2034 291.5236 0057084 64.2430 59.9261 14.07973493953079

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
CZ-6A DEB LEO 2025-08-04 09:03:28 0.0002275606 348.0 (m) DEBRIS
SL-16 R/B LEO 2025-06-30 03:01:10 0.0005681265 24.0 (m) ROCKET BODY
METEOR 1-11 LEO 2025-03-19 04:05:04 0.0001090281 573.0 (m) PAYLOAD
FENGYUN 1C DEB SSO 2024-09-12 06:34:40 0.0001874561 101.0 (m) DEBRIS
THORAD AGENA D DEB LEO 2024-08-15 17:15:53 0.0001778222 354.0 (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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