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
- 437325000.0
- Baud
- 19200
- IARU Coordination
- IARU Coordinated
Mode U - GFSK9k6 - AX.25 G3RUH
- Type
- Transmitter
- Service
- Amateur
- Downlink Mode
- GFSK
- Downlink Frequency
- 437325000.0
- Baud
- 9600
- IARU Coordination
- IARU Coordinated
Mode S - OQPSK 10Mbps - CCSDS
- Type
- Transmitter
- Service
- Amateur
- Downlink Mode
- OQPSK
- Downlink Frequency
- 2405000000.0
- Baud
- 10000000
- IARU Coordination
- IARU Coordinated
Mode S - OQPSK 5Mbps - CCSDS
- Type
- Transmitter
- Service
- Amateur
- Downlink Mode
- OQPSK
- Downlink Frequency
- 2405000000.0
- Baud
- 5000000
- IARU Coordination
- IARU Coordinated
Most Recent Observers (last 24h)
| Observer | Latest Data |
|---|---|
| UX5UL-KO50ei | 2026-10-01 13:00:32 UTC |
| Apomahon-KM18ub | 2026-10-01 12:53:48 UTC |
| VA3ROM-EN58jk | 2026-10-01 10:07:52 UTC |
| VU2JEK_Nitin-MK83sd | 2026-10-01 09:38:55 UTC |
| JF6FYI Nishikazu, KitaKyushu, 3-ele Yagi(UHF)-PM53kv | 2026-10-01 06:32:26 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
- 2026-10-01 11:23:45 UTC
- TLE Set
-
1 68506U 26067CU 26273.87229889 .00003678 00000-0 17207-3 0 9993
2 68506 97.4638 231.0746 0004947 80.9051 279.2744 15.20372052 27870