MaSat-1
Mission type | Technology |
---|---|
Operator | Technical University of Budapest |
COSPAR ID | 2012-006E ![]() |
SATCAT no. | 38081 |
Website | http://cubesat.bme.hu/?lang=en |
Mission duration | 3 months |
Spacecraft properties | |
Spacecraft type | 1U CubeSat |
Launch mass | 1 kilogram (2.2 lb) |
Power | watts |
Start of mission | |
Launch date | 13 February 2012, 10:00:00 (2012-02-13UTC10Z) UTC[1] |
Rocket | Vega VV01 |
Launch site | Kourou ELA-1 |
Contractor | Arianespace |
End of mission | |
Last contact | 9 January 2015, 21:21:43 (2015-01-09UTC21:21:44Z) [2] |
Orbital parameters | |
Reference system | Geocentric |
Regime | Low Earth |
Perigee altitude | 302 kilometres (188 mi) |
Apogee altitude | 1,071 kilometres (665 mi) |
Inclination | 69.47 degrees |
Period | 98.35 minutes |
Epoch | 9 November 2013, 01:42:56 UTC[3] |
MaSat-1 (from the words Magyar and Satellite, the first meaning "Hungarian" in Hungarian, maszat, pronounced IPA [ˈmɒsɒt], meaning "smudge") is the first indigenous Hungarian satellite, developed and built by students at the Technical University of Budapest. The 1U CubeSat-type satellite was launched into low Earth orbit on 13 February 2012. The satellite provided telemetric data as well as VGA resolution color images at the 70 cm amateur radio wavelength (437.345 MHz frequency) received at the tracking center at Budapest. The center was tested on 31 March 2009 with the help of Charles Simonyi on board the International Space Station. With the successful launch of MaSat-1, Hungary became the 47th nation to orbit a satellite.[4] Between 9 and 10 January 2015, the satellite reentered into the atmosphere.[5]
Operations
Weeks following its launch, after the first high-quality images were available was it revealed to the public that a camera was on board.
Technical specifications
- Satellite class: 1U CubeSat
- Dimensions: 10 cm × 10 cm ×10 cm
- Mass: 1 kg
- Propulsion: no
- Expected life: minimum 3 months
- Input power: 1.2 – 2.2 W
- Communication type: Half-duplex
- Frequency: 437,345 MHz
- Data rate: 625 or 1250 bps
- Modulation: 2-GFSK
- Transmission power: 100/400 mW
- Telemetry protocol: modified ESA PUS v1
- Callsign: HA5MASAT
- Digital camera: VGA sensor, 640×480 pixels
[6]
See also
References
- ^ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 9 November 2013.
- ^ Nem küld több jelet a Masat-1
- ^ Peat, Chris (9 November 2013). "MaSat-1 - Orbit". Heavens Above. Retrieved 9 November 2013.
- ^ "Hungary Becomes Space Nation « ADAM MAJOROSI". Archived from the original on 2012-03-07. Retrieved 2012-02-15. As of 25 November 2012, MaSat-1 remains in orbit.
- ^ Nem küld több jelet a Masat-1
- ^ Source: http://www.urvilag.hu/article.php?id=2984 (Hungarian)
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- Navid
- LARES, ALMASat-1, Xatcobeo, UniCubeSat-GG, ROBUSTA, e-st@r, Goliat, MaSat-1, PW-Sat
- SES-4
- Compass-G5
- MUOS-1
- Edoardo Amaldi ATV
- Intelsat 22
- Kosmos 2479
- Apstar 7
- USA-234
- Kwangmyŏngsŏng-3
- Progress M-15M
- YahSat-1B
- RISAT-1
- Compass-M3, Compass-M4
- USA-235
- Tianhui 1B
- Yaogan 14, Tiantuo 1
- Soyuz TMA-04M
- JCSAT-13, Vinasat-2
- Kosmos 2480
- Shizuku, Kompsat 3, SDS-4, Horyu 2
- Nimiq 6
- SpaceX COTS Demo Flight 2, New Frontier
- Fajr
- ChinaSat 2A
- Yaogan 15
- Intelsat 19
- NuSTAR
- Shenzhou 9
- USA-236 / Quasar 18
- USA-237 / Orion 8
- EchoStar XVII, MSG-3
- SES-5
- Soyuz TMA-05M
- Kounotori 3 (Raiko, We-Wish, Niwaka, TechEdSat, F-1)
- Kanopus-V1, BelKA-2, Zond-PP, TET-1, exactView-1
- Tianlian I-03
- Gonets-M No.3, Gonets-M No.4, Kosmos 2481, MiR
- Progress M-16M (Sfera-53)
- Intelsat 20, HYLAS 2
- Telkom-3, Ekspress-MD2
- Intelsat 21
- RBSP-A, RBSP-B
- USA-239
- SpaceX CRS-1, Orbcomm-2
- David, Sif
- Shijian 9-01, Shijian 9-02
- Intelsat 23
- Soyuz TMA-06M
- Compass G6
- Progress M-17M
Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).
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