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Long March 4C

Long March familyChina Aerospace Science and Technology CorporationActive

The Long March 4C, also known as the Chang Zheng 4C, CZ-4C and LM-4C, previously designated Long March 4B-II, is a Chinese orbital carrier rocket. It is launched from the Jiuquan, Taiyuan Satellite Launch Centre and Xichangs, and consists of 3 stages. Long March 4C vehicles have been used to launch the Yaogan-1, Yaogan-3 SAR satellites and the Fengyun-3A polar orbiting meteorological satellite. On December 15, 2009 a Long March 4C was used to launch Yaogan 8.

Long March 4C vehicle

Specifications

Thrust
2,962 kN
Height
45.8 m
Diameter
3.35 m
Launch mass
250 t
Stages
3
LEO capacity
4,200 kg
GTO capacity
1,500 kg
SSO capacity
2,800 kg

Specifications from Launch Library. Figures the operator has not published are omitted.

Flight record

60flightswith a definitive outcome
96.7%success rate58 of 60
2failuresincluding partial failures
34success streakcurrent

First flight April 26, 2006 · latest April 17, 2026 · 04:10 UTC

Counted from padside's own launch record, the same basis as the stats page.

Flights per year

  • Successful
  • Failed
Show the numbers for Long March 4C flights per year
Long March 4C flights per year
YearSuccessfulFailedTotal
2006101
2007101
2008101
2009101
2010303
2011000
2012202
2013404
2014303
2015202
2016112
2017101
2018404
2019213
2020101
2021909
202210010
2023606
2024202
2025303
2026101

Flights

5 of 60

All 60 flights