CZ-4 DEB

Satellite information

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Satellite Type and Status

DEBRISIN ORBIT

Key statistics

Satellite CZ-4 DEB at a glance.

Uptime

12725

Days in orbit

Revolutions

≈ 14.2

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

98.7

Latest

Satellite identification and parameters

Extended collection of information and parameters for CZ-4 DEB.

Object identification

Identified? True

Debris? True

Object name: CZ-4 DEB

International designator: 1990-081F

Object number (NORAD): 20793

Object ID (CCSDS): 20793

Country: PEOPLES REPUBLIC OF CHINA (PRC)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 101.399 minutes

Inclination: 98.7409 deg

SMA: 7203.06 km

Apoapsis: 837.893 km

Periapsis: 811.958 km

RAAN: 173.07 deg

Eccentricy: 0.0018003

Argument of periapsis: 256.5695 deg

Mean anomaly: 156.6098 deg

Mean motion: 14.2012699 rev/day

Mean motion (dot): 0.00000374 rev/day2

B* drag term: 0.00019572 1/REarth

Two-line elements (TLE)

Creation date: July 5, 2025, 10:46 p.m.

Reference frame: TEME

Reference center: EARTH

Epoch: July 5, 2025, 10:03 p.m. UTC

TLE line 0: 0 CZ-4 DEB

TLE line 1: 1 20793U 90081F 25186.91909044 .00000374 00000-0 19572-3 0 9998

TLE line 2: 2 20793 98.7409 173.0700 0018003 256.5695 156.6098 14.20126990794603

Live tracking on map

Real-time ground track for satellite CZ-4 DEB.

In-orbit conjunctions

A list of the most updated potential collisions computed for object CZ-4 DEB.

Target Orbit TCA Probability of collision Miss distance Type
FENGYUN 1C DEB SSO 2025-06-25 15:20:46 0.0004059259 148.0 (m) DEBRIS
BLITS SSO 2025-06-12 13:41:24 0.0001783481 537.0 (m) PAYLOAD
FENGYUN 1C DEB SSO 2025-03-20 04:33:37 0.0001342918 168.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2025-03-05 19:31:10 0.0001139455 101.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2024-10-26 11:28:27 0.0001015089 305.0 (m) DEBRIS

Associated space launch

Chinese polar orbiting meteorological satellite

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

The launch took place on Sept. 3, 1990, 12:53 a.m. from Launch Complex 7.

For more information about the launch, click the button.

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

Agency: N/A

Status: Launch Successful

Launch date: Sept. 3, 1990, 12:53 a.m. UTC

Rocket: Long March 4A

Launch pad: Launch Complex 7

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

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