XY 2 & Others

Launch Success

Liftoff Time (GMT)

23:01:00

Saturday September 19, 2015

Mission Details

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Launch Notes

First flight of Long March 6.

Zheda Pixing 2A & 2B

Wiki

ZDPS-2 is a nano-satellite mission of the Microsat Research Center, Zhejiang University, which performs an in-orbit test for formation flying technology with two identical nano-satellites, ZDPS-2A and ZDPS-2B. Both satellites carried a deployable structure experiment, which was unfolded in orbit. ZDPS-2A and B are both equipped with a propulsion system, either of them can be treated as chief or deputy. The system uses liquid ammonia as a propellant with ISP greater than 900 Ns/kg. With a fuel mass of 0.318 kg and a satellite mass of below 12 kg, the system can provide a total ΔV of 24 m/s.

Low Earth Orbit

2 Payloads

24 kilograms

LilacSat 2

Wiki

CAS 3H or LilacSat 2 is a low-cost, nano-satellite for education, amateur radio communication, and technology demonstration, built by a team of 15 students of Harbin Institute of Technology (HIT). It is a cube-shaped 20 cm × 20 cm × 20 cm satellite with a weight of 11 kg. LilacSat-2 provides hands-on experience for students who would not otherwise have the opportunity to build flight hardware for a space mission. The training these students gain by working on this project will better prepare them for work in the aerospace industry.

Low Earth Orbit

1 Payload

11 kilograms

Naxing 2

Wiki

NS-2 (Nano Satellite 2) on Naxing 2, a Chinese nano- or micro-satellite developed by Tsinghua University. The satellite will evaluate various new satellite components like micro star trackers, micro sun sensors, MEMS gyroscopes and magnetometers, quartz tuning fork sensors, and GPS/BDS navigation receivers. NS 2 carries two nanosatellites, ZJ 1 and KJSY 1, to be deployed in orbit.

Low Earth Orbit

3 Payloads

20 kilograms

Luliang 1

Wiki

The TT 3 (Tiantuo 3) is a small satellite built by the National University of Defense Technology (NUDT). The satellite performs technology demonstrations. The main payloads are a spaceborne Automatic Identification System (AIS) signal receiver, a spaceborne aviation target signal automatic dependent surveillance-broadcast (ADS-B) signal receiver, and a fire monitoring payload.

Low Earth Orbit

1 Payload

XY 2

Wiki

XY 2 (Xinyan-2 or NewTech-2) is a Chinese microsatellite to test new technologies in space. XY 2 is a test bed for an electric propulsion system.

Low Earth Orbit

1 Payload

130 kilograms

DCBB

Wiki

DCBB or CAS 3G (Chinese Amateur Radio satellite 3G) is a 2U Cubesat for University educational purposes designed by Shenzhen Aerospace Dongfanghong HIT Satellite Ltd. together with CAMSAT.

Low Earth Orbit

1 Payload

XC 1, 2, 3, 4

Wiki

Xingchen or XS series consists of four small satellites built by the National University of Defense Technology (NUDT). The Xingchen picosatellites have the dimensions of 98 mm × 98 mm × 7 mm and a weight of 100 g. The four satellites will fly in formation with TT-3 and NUDT-PhoneSat to test out inter-satellite communication techniques. Two of the four will be controlled by TT-3 and the other two by PhoneSat. The main satellite will also track ship AIS and airplane signals.

Low Earth Orbit

4 Payloads

1 kilograms

XW 2A to 2F

Wiki

XW 2A, 2B, 2C, 2D, 2E, and 2F are a constellation of three identical Chinese micro-satellite for atmospheric physics experiments and amateur radio missions. The satellites feature a 246 mm × 246 mm × 246 mm cubic body with body-mounted solar cells and a mass of approximately 10 kg mass. They feature a three-axis stabilization system. The amateur communications payload consists of U/V 20 kHz wide transponders with 145 MHz CW beacon and 19k2 GMSK AX25 telemetry downlinks.

Low Earth Orbit

5 Payloads

57 kilograms

NUDT-PhoneSat

Wiki

NUDT-PhoneSat or CAS 3I (Chinese Amateur Radio satellite 3I) is a Chinese experimental pico satellite developed by the National University of Defense Technology and CAMSAT. The satellite is based on smartphone technology.

Low Earth Orbit

1 Payload

1 kilograms

Rocket

Active
Long March 6

Active Since 2015

China Aerospace Science and Technology Corporation logo

Agency

CASC

Price

$19.00 million

Rocket

Height: 29.24m

Payload to Orbit

LEO: 1,080 kg

GTO: 0 kg

Liftoff Thrust

1,188 Kilonewtons

Fairing

Diameter: 2.6m

Height: 6.145m

Stages

3

Launch Site

LC-16

Taiyuan Satellite Launch Center, China

Fastest Turnaround

24 days 2 hours

Stats

Long March 6


1st

Mission

1st

Mission of 2015

2015


52nd

Orbital launch attempt