VELOX I

Nanyang Technological University VELOX-I

VELOX-I is the first Singapore nanosatellite to operate in Low Earth’s Orbit (LEO). It is part of NTU’s Undergraduate Satellite Program, which provides an opportunity for engineering students to participate in a multidisciplinary hands-on space project. Besides educational objective, VELOX-I also contributes to the nanosatellite research with its technology demonstration and scientific payloads.


NASA-Catalog: 40057

Downlink

145.980 MHZ CW beacon

Call

VELOXP

Status

INACTIVE

Orbital Parameter

NORAD                   40057
COSPAR designator       2014-034-E  
Inclination             98.249
RA of A. Node           305.916
Eccentricity            0.0013449
Argument of Perigee     101.412
Revs per day            14.74068384
Period                  1h 37m 41s (97.68 min)
Semi-major axis         7 026 km
Perigee x Apogee        639 x 658 km
BStar (drag term)       0.000178070 1/ER
Mean anomaly            258.860



Mission Objectives


Telemetry

sveloxi 2qqggcdddd2ygdj82dff
sveloxi 2qqggdfdfd2ygdj82ddd
sveloxi 2qqggdfffd2ygdja2fdf
sveloxi 2qqggfgfgd2ygdja2dfd
sveloxi 2qqggfgfgd2ygdja2fff
sveloxi 2qqggggggd2ygdja2dfd
sveloxi 2qqgggjgjd2ygdja2dff
sveloxi 2qqgggjgjd2ygdja2dff
sveloxi 2qqggjjjjd2ygdja2fff
sveloxi 2qqggjjjjd2ygdja2ffd

veloxi_18072014

Links und weitere Informationen

http://www.sarc.eee.ntu.edu.sg/Research/Projects/Pages/VELOX-I.aspx

VELOX P-II

Nanyang Technological University VELOX-PII

VELOX-PII (Picosatellite II) is the first CubeSat of SaRC (Satellite Research Center) at NTU (Nanyang Technological University), Singapore. VELOX-PII is a 1U CubeSat with a mass of 1.33 kg and dimensions of 10 cm x 10 cm x 11.35 cm. The CubeSat structure uses a hard anodized Al. 7075 chassis, with stainless steel load bearing parts.
The CubeSat is 3-axis stabilized. The ADCS (Attitude Determination and Control Subsystem) features 1 GPS receiver, 2 IMUs (Inertial Measurement Units), 1 dual-FOV sun sensor, 5 coarse sun sensors, and 3 magnetic torquers.


NASA-Catalog: 39438

Downlink

145.980 MHZ CW beacon

Call

VELOXP

Status

inactive

Orbital Parameter

NORAD                   39438
COSPAR designator       2013-066-Y  
Inclination             97.766
RA of A. Node           304.167
Eccentricity            0.0074832
Argument of Perigee     22.042
Revs per day            14.75516180
Period                  1h 37m 35s (97.58 min)
Semi-major axis         7 022 km
Perigee x Apogee        591 x 696 km
BStar (drag term)       0.000107250 1/ER
Mean anomaly            338.399

Telemetry

22:53 UTC veloxp gz8d8cgd22222
22:54 UTC veloxp gz8d8cgd22222
22:55 UTC veloxp gz8dqcgd22222
22:56 UTC veloxp gz8dqcgd22222
22:57 UTC veloxp gz8dqcgd22222
22:58 UTC veloxp gz8dqcgdf2222
22:59 UTC veloxp gz8dqcgdf2222
23:00 UTC veloxp gz8dqcgdf22ff
23:01 UTC veloxp gz8dqcgdf22ff
23:02 UTC veloxp gz8dqcgdff2ff
G LEOP Idle Mode
Z Battery State of Charge > 90%
8 Battery Voltage > 8.2 V
C Battery Temp 0°C .. 5°C
G ADCS Subsystem’s MCU Temperature 0°C .. 15 °C
D -
2 Solar Panel 1 Temperature -30°C .. -10°C
2 Solar Panel 2 Temperature -30°C .. -10°C
2 Solar Panel 3 Temperature -30°C .. -10°C
2 Solar Panel 4 Temperature -30°C .. -10°C
2 Solar Panel 5 Temperature -30°C .. -10°C
22.11.2013 - first telemetry (DK3WN)
velox_02122013

Links und weitere Informationen

https://directory.eoportal.org/web/eoportal/satellite-missions/v-w-x-y-z/velox-pii
http://www.sarc.eee.ntu.edu.sg/Research/Projects/Pages/VELOX-P.aspx

Launch

A Dnepr launch vehicle blasted off from the Dombarovsky Air Base, Orenburg Region, Russia, on November 21, 2013 at 7:10 UTC carrying a total of 32 spacecraft of different shapes and sizes to orbit. The launch was successful and all satellites were released into their desired orbits.



tagesaktuelle Telemetriedaten ...

DK3WN SatBlog