METEOR M2-4
Mission information
- Name
- METEOR M2-4
- Alternate Names
- METEOR 2 2-4, METEOR-M N2-4
- Satellite ID
- VSVI-4798-5613-4587-2414
- NORAD ID
- 59051
- Country of Origin
-
Russia
Status
Operational
Satellite is in orbit and operational
Image
Mission timeline
- Launch Date
- 2024-02-29T05:43:26+00:00
Description
Meteorology satellite
SatNOGS Links
LRPT S-E RHCP D 80 kbps
- Type
- Transmitter
- Service
- Meteorological
- Downlink Mode
- LRPT
- Downlink Frequency
- 137912500
- Baud
- 80000
LRPT S-E RHCP D 80 kbps
- Type
- Transmitter
- Service
- Meteorological
- Downlink Mode
- LRPT
- Downlink Frequency
- 137900000
- Baud
- 80000
LRPT S-E RHCP D 80 kbps
- Type
- Transmitter
- Service
- Meteorological
- Downlink Mode
- LRPT
- Downlink Frequency
- 137100000
- Baud
- 80000
HRPT
- Type
- Transmitter
- Service
- Meteorological
- Downlink Mode
- HRPT
- Downlink Frequency
- 1705000000
- Baud
- 3000000
HRPT
- Type
- Transmitter
- Service
- Meteorological
- Downlink Mode
- HRPT
- Downlink Frequency
- 1700000000
- Baud
- 3000000
LRPT IQ recording usage
- Type
- Transmitter
- Service
- Meteorological
- Downlink Mode
- FSK
- Downlink Frequency
- 137100000
- Baud
- 40000
- Unconfirmed
- Yes
SARSAT L-band
- Type
- Transmitter
- Downlink Mode
- BPSK
- Downlink Frequency
- 1544500000
- Baud
- 100000
LRPT S-E RHCP D 72 kbps
- Type
- Transmitter
- Service
- Meteorological
- Downlink Mode
- LRPT
- Downlink Frequency
- 137100000
- Baud
- 72000
LRPT S-E RHCP D 72 kbps
- Type
- Transmitter
- Service
- Meteorological
- Downlink Mode
- LRPT
- Downlink Frequency
- 137900000
- Baud
- 72000
LRPT IQ recording usage
- Type
- Transmitter
- Service
- Meteorological
- Downlink Mode
- FSK
- Downlink Frequency
- 137900000
- Baud
- 40000
Most Recent Observers (last 24h)
| Observer | Latest Data |
|---|---|
| I LOVE BALI-OI71ng | 2026-03-27 07:15:18 UTC |
| CGBSAT-VHF-JO32eu | 2026-03-27 04:31:29 UTC |
Data Frames Decoded - 30 Days
There is no decoded data for this satellite in the last 30
days.
No Decoders Found
Help us develop a decoder, you can find instructions at this wiki link
Orbital Elements
Latest Two-Line Element (TLE)
- TLE Source
- Space-Track.org
- TLE Updated
- 2026-03-27 05:19:43 UTC
- TLE Set
-
1 59051U 24039A 26085.95339583 .00000051 00000-0 42632-4 0 9991
2 59051 98.6933 46.3213 0008002 53.1145 307.0765 14.22419868107571