HXMT, ÑuSat 3, Zhuhai-1 OVS 1A & 1B

Launch Success

Liftoff Time (GMT)

03:00:00

Thursday June 15, 2017

Watch Replay

Official Livestream

Mission Details

Read Article

HXMT

Wiki

HXMT (Hard X-ray Modulation Telescope) is a collimated hard X-ray (20-200 keV) telescope with high sensitivity and spatial resolution. It is a collaboration between institutes in China (which will provide the spacecraft and main hard X-ray imager) and the UK (which will provide low and medium-energy imaging instruments).

Sun-Synchronous Orbit

1 Payload

2,500 kilograms

ÑuSat 3

Wiki

The Argentinian ÑuSat earth observation satellites form the Aleph-1 constellation developed and operated by Satellogic S.A. The satellites in the constellation are identical 51 cm × 57 cm × 82 cm spacecraft of 37.5 kg mass. The satellites are equipped with an imaging system operating in visible light and infrared. The constellation will allow for commercially available real-time Earth imaging and video with a ground resolution of 1 m. The satellites were developed based on the experience gained on the BugSat 1 (Tita) prototype satellite. A U/V transponder with 2 W of output power for 8 GHz downlink and 2 GHz uplink will be operating on 100 kHz bandwidth. For backup telemetry, designers are considering UHF transponder operating at 9k6 GFSK.

Sun-Synchronous Orbit

1 Payload

38 kilograms

Zhuhai-1 OVS 1A & 1B

Wiki

The Zhuhai-1 earth observation satellites are the video component of the Chinese Orbita earth observation system by Zhuhai Orbita Control Engineering Ltd. Two OVS-1 satellites will constitute the prototype OVS-1 video component. The operational Orbita constellation is to consist of ten video satellites (OVS-2), hyperspectral satellites (OHS-2), and small personal satellites (OPS-2).

Sun-Synchronous Orbit

2 Payloads

100 kilograms

Rocket

Active
Long March 4B

Active Since 1999

China Aerospace Science and Technology Corporation logo

Agency

CASC

Price

$64.68 million

Rocket

Height: 46.97m

Payload to Orbit

LEO: 4,200 kg

GTO: 1,500 kg

Liftoff Thrust

2,993 Kilonewtons

Fairing

Diameter: 3.8m

Height: 11.74m

Stages

3

Launch Site

Site 9401 (SLS-2)

Jiuquan Satellite Launch Center, China

Fastest Turnaround

10 days 18 hours

Stats

Long March 4B


29th

Mission

1st

Mission of 2017

2017


36th

Orbital launch attempt