Microspace Rapid Pte Ltd, Singapore
POPSAT-HIP-1 is an triple cubesat. The spacecraft is to demonstrate the functionality of a high resolution optical payload and attitude control propulsion system on a Cubesat class Nanosatellite.
NASA-Catalog: 40028
Downlink
437.405 MHz FM 1k2 AFSK, 9k6 FSK AX.25, CW
Call
POPSAT-HIP1
Status
INACTIVE
Orbital Parameter
NORAD 40028 COSPAR designator 2014-033-U Inclination 97.978 RA of A. Node 132.592 Eccentricity 0.0016624 Argument of Perigee 69.170 Revs per day 14.85187590 Period 1h 36m 57s (96.95 min) Semi-major axis 6 991 km Perigee x Apogee 601 x 625 km BStar (drag term) 0.000135820 1/ER Mean anomaly 291.132
Telemetry
popsat-hip1 7.08v 33c 23c popsat-hip1 7.07v 33c 23c popsat-hip1 7.06v 34c 23c popsat-hip1 7.04v 34c 24c popsat-hip1 7.04v 32c 25c popsat-hip1 7.07v 33c 25c popsat-hip1 7.09v 34c 25c popsat-hip1 7.10v 36c 25c popsat-hip1 7.09v 36c 26c popsat-hip1 7.10v 37c 26c popsat-hip1 7.11v 37c 27c popsat-hip1 7.10v 38c 27c popsat-hip1 7.08v 39c 28c popsat-hip1 7.08v 39c 29c
22.08.2014, 09:18 UTC CW beacon
Links und weitere Informationen
Launch
The liftoff of the 20th Dnepr rocket, took place as scheduled on June 19, 2014, at 19:11:11 UTC from an underground silo facility No. 370/13 in the Dombarosvsky ICBM deployment area in southern Russia. The rocket carried the KazEOSat-2 (DZZ-MRES) remote-sensing satellite for the imaging of the Earth surface, which was built by the European consortium Airbus Defense and Space for the government of Kazakhstan and a cluster of 36 secondary payloads for customers from 17 countries, including Deimos-2, Hodoyoshi-3, Hodoyoshi-4, BugSat-1, SaudiSat-4, AprizeSat-9, AprizeSat-10, UniSat-6, Tigrisat, AeroCube 6, ANTELSAT, Lemur-1, BRITE-CA 1, BRITE-CA 2, NanosatC-Br1, Duchifat-1, Perseus-M1, Perseus-M2, QB50P1, QB50P, Tablesat-Avrora, 11 satellites Flock-1c, POPSAT-HIP 1, PACE, PolyITAN, DTUSat-2.