AEPEX
Mission information
- Name
- AEPEX
- Satellite ID
- ROGL-5396-9562-5275-1160
- NORAD ID
- 68506
- Associated Satellites
-
RFCC-7272-3583-0134-2315
- Website
- https://lasp.colorado.edu/missions/aepex/
- Country of Origin
-
United States of America
Status
Operational
Satellite is in orbit
Reception
Image
Mission timeline
- Launch Date
- 2026-03-30T11:02:00+00:00
Description
AEPEX (Atmospheric Effects of Precipitation through Energetic X-Rays) is a 6U CubeSat that will study radiation belt losses through energetic particle precipitation (EPP) in the upper atmosphere, magnetopause shadowing, and wave-particle interactions. It uses a novel method to distinguish and quantify the impacts of these different components by measuring flux, spectrum, spatial scales, and temporal scales of EPP.
SatNOGS Links
Mode U - GFSK19k2 - AX.25 G3RUH
- Type
- Transmitter
- Service
- Amateur
- Downlink Mode
- GFSK
- Downlink Frequency
- 437325000
- Baud
- 19200
- IARU Coordination
- IARU Coordinated
Mode U - GFSK9k6 - AX.25 G3RUH
- Type
- Transmitter
- Service
- Amateur
- Downlink Mode
- GFSK
- Downlink Frequency
- 437325000
- Baud
- 9600
- IARU Coordination
- IARU Coordinated
Mode S - OQPSK 10Mbps - CCSDS
- Type
- Transmitter
- Service
- Amateur
- Downlink Mode
- OQPSK
- Downlink Frequency
- 2405000000
- Baud
- 10000000
- IARU Coordination
- IARU Coordinated
Mode S - OQPSK 5Mbps - CCSDS
- Type
- Transmitter
- Service
- Amateur
- Downlink Mode
- OQPSK
- Downlink Frequency
- 2405000000
- Baud
- 5000000
- IARU Coordination
- IARU Coordinated
Most Recent Observers (last 24h)
| Observer | Latest Data |
|---|---|
| MAUSyagi-DN70ja | 2026-09-09 22:50:11 UTC |
| JF6FYI Nishikazu, KitaKyushu, 3-ele Yagi(UHF)-PM53kv | 2026-09-09 18:32:54 UTC |
| Peters-GS1-PM37ki | 2026-09-09 18:31:18 UTC |
| JF6FYI Nishikazu, KitaKyushu, QFH (UHF)-PM53kv | 2026-09-09 18:30:52 UTC |
| ZL2TAY-RE79md | 2026-09-09 15:42:56 UTC |
Data Frames Decoded - 30 Days
There is no decoded data for this satellite in the last 30
days.
Decoder: AEPEX Telemetry
- Script Name
- aepex
- Decoder Fields
- Click here
Orbital Elements
Latest Two-Line Element (TLE)
- TLE Source
- Space-Track.org
- TLE Updated
- 2026-09-09 17:20:02 UTC
- TLE Set
-
1 68506U 26067CU 26252.41488036 .00006264 00000-0 29274-3 0 9992
2 68506 97.4590 209.8430 0004273 126.6556 233.5072 15.20140419 24616