Meteor-M No.2
Mission type | Weather |
---|---|
Operator | Roscosmos/Roshydromet |
COSPAR ID | 2014-037A |
SATCAT no. | 40069 |
Spacecraft properties | |
Launch mass | 2,700 kilograms (6,000 lb) |
Start of mission | |
Launch date | 8 July 2014 (2014-07-08) |
Launch site | Baikonur |
Orbital parameters | |
Reference system | Geocentric |
Regime | Sun-synchronous |
Perigee altitude | 825.5 kilometres (512.9 mi)[1] |
Apogee altitude | 835.0 kilometres (518.8 mi)[1] |
Inclination | 98.5 degrees[1] |
Period | 101.4 minutes[1] |
Meteor ← Meteor-M No.1 Meteor-M No.2-1 → |
Meteor-M No.2 (also known as Meteor M2) was the second Russian Meteor-M series of polar-orbit weather satellite.[1] It was launched on a Soyuz-2.1b rocket with a Fregat upper stage on 8 July 2014. It was designed to operate for 5 years.[1]
See also
- Meteor
References
- ^ a b c d e f "METEOR M2 satellite details". N2YO.com - Real Time Satellite Tracking and Predictions. Retrieved 2019-08-20.
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← 2013
Orbital launches in 20142015 →
- Kosmos 2495
- Ekspress AM4R
- USA-251
- USA-252
- Kosmos 2496, Kosmos 2497, Kosmos 2498, Kosmos 2499
- ALOS-2, Raijin-2, UNIFORM-1, SOCRATES, SPROUT
- Eutelsat 3B
- Soyuz TMA-13M
- Kosmos 2500 / GLONASS-M 755
- AprizeSat 9, AprizeSat 10, BRITE-Montreal, BRITE-Toronto, BugSat 1, Deimos-2, Hodoyoshi 3, Hodoyoshi 4, KazEOSat 2, Perseus-M1, Perseus-M2, SaudiSat-4, TabletSat-Aurora, UniSat-6 (Lemur-1, Tigrisat), Flock-1c × 11
- SPOT 7, CanX-4, CanX-5
- OCO-2
- Gonets-M × 3
- Meteor-M No.2
- O3b × 4
- CRS Orb-2 (Flock-1b × 28, TechEdSat-4)
- Orbcomm-OG2 × 6
- Foton-M No.4
- Progress M-24M
- USA-253 / GSSAP 1, USA-254 / GSSAP 2, USA-255 / ANGELS
- Georges Lemaître ATV
- USA-256
- AsiaSat 8
- Yaogan 20 A, B, C
- WorldView-3
- Gaofen 2, Heweliusz
- Galileo FOC-1, Galileo FOC-2
- Chuangxin 1-04, Lingqiao
- AsiaSat 6
- Yaogan 21, Tiantuo 2
- MEASAT 3b, Optus 10
- USA-257
- SpaceX CRS-4
- Soyuz TMA-14M
- Olimp-K
- Shijian XI-07
- Himawari 8
- IRNSS-1C
- ARSAT-1, Intelsat 30
- Yaogan 22
- Ekspress AM6
- Chang'e 5-T1, 4M
- Shijian 11-08
- Cygnus CRS Orb-3† (Arkyd-3†, Flock-1d × 26†)
- Progress M-25M
- USA-258 / GPS IIF 8
- Meridian 7
- Sasuke, Hodoyoshi 1, Kinshachi 1, Tsukushi, TSUBAME
- Yaogan 23
- Yaogan 24
- Kuaizhou 2
- Soyuz TMA-15M
- Kosmos 2501
- Hayabusa2, PROCYON, Shinen 2, DESPATCH
- Orion EFT-1
- DirecTV-14, GSAT-16
- CBERS-4
- Yaogan 25 A, B, C
- USA-259
- Yamal-401
- O3b × 4 (FM9 to FM12)
- Kondor-E No.2
- IPM
- Kosmos 2502
- Resurs-P No.2
- Yaogan 26
- Astra 2G
- Fengyun 2-08
Launches are separated by dots ( • ), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ).
Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).
Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).
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