ALMASat-1
| Jenis misi | Teknologi |
|---|---|
| Operator | Universitas Bologna |
| COSPAR ID | 2012-006B |
| SATCAT no. | 38078 |
| Properti wahana | |
| Massa luncur | 125 kilogram (276 pon) |
| Dimensi | 30 sentimeter (12 in) cube |
| Awal misi | |
| Tanggal luncur | 13 Februari 2012, 10:00:00 UTC |
| Roket peluncur | Vega |
| Tempat peluncuran | Kourou ELA-1 |
| Kontraktor | Arianespace |
| Parameter orbit | |
| Sistem rujukan | Geosentrik |
| Sistem orbit | Bumi rendah |
| Ketinggian perigee | 311 kilometer (193 mi) |
| Ketinggian apoogee | 1.250 kilometer (780 mi) |
| Inklinasi | 69,5 derajat |
| Periode | 100,32 menit |
| Epoch | 19 Desember 2013, 04:49:04 UTC[1] |
ALMASat-1 (Almamater Satellite) adalah sebuah satelit mikro yang dikembangkan oleh Universitas Bologna untuk keperluan demonstratif yang akan membantu misi pengamatan bumi. Proyek ini didanai oleh Kementerian Riset Italia.
Rujukan
- ^ "ALMASAT-1 Satellite details 2012-006B NORAD 38078". N2YO. 19 December 2013. Diakses tanggal 20 December 2013.
- ALma MAter SATellite Official Site
- ALMASAT at European Space Agency Diarsipkan 2012-02-20 di Wayback Machine.
 | Artikel bertopik roket ini adalah sebuah rintisan. Anda dapat membantu Wikipedia dengan mengembangkannya. |
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