POPSAT-HIP 1 satellite

POPSAT-HIP 1

Singapore

Spacecraft nº:

Singapore spacecraft nº: 5

Launch data:

Designation	40028 / 14033U
Launch date	19 June 2014 - 19:11 UT
Launch site	Dombarovsky, LC-370/13
Launch vehicle	Dnepr
Mission	Technology
Earth orbit:
Perigee / Apogee	607 x 629 km
Eccentricity
Inclination	98.0°
Period	96.9 min

Launched together with: Deimos 2 - KazEOSat 2 - TabletSat-Aurora - BugSat 1 - SaudiSat 4 - Hodoyoshi 3 - Hodoyoshi 4 - AprizeSat 9 - AprizeSat 10 - UniSat 6 - BRITE-CA 1 - BRITE-CA 2 - Perseus-M 1 - Perseus-M 2 - Flock-1c 1-11 - Tigrisat - Lemur 1 - QB50P1 - QB50P2 - PACE - ANTELSAT - DTUSat 2 - Duchifat 1 - NanoSatC-Br 1 - PolyITAN 1 - AeroCube 6A - AeroCube 6B

Spacecraft data:

Prime manufacturer	Microspace Rapid Pte Ltd.
Platform	CubeSat (3U)
Operator	Microspace Rapid Pte Ltd.
Mass at launch	3 kg
Dry Mass	kg
Basic shape
Dimension (m)
Equipment
Solar array	Solar cells
Stabilization
Propulsion
DC power
Design lifetime

Description:

POPSAT-HIP 1 is a triple cubesat built by Microspace Rapid Pte Ltd., Singapore. The spacecraft is to demonstrate the functionality of a high resolution optical payload and attitude control propulsion system on a Cubesat Class Nano-satellite.

Mission details:

On Jun 19, 2014 launch of a Dnepr rocket from the Yasniy missile base put a record 38 payloads in sun-synchronous orbits ranging from 550 to 610 km at perigee and 620 to 715 km at apogee.
POPSAT-HIP1 is a 3U cubesat from Microspace Rapid in Singapore.

External links:

Satellite tracking:
Real time satellite tracking

Ref.: #7(JR699), #14, #228 - update: 03.12.14