SINP-MSU-80 (Scorpion)
Mission information
Name
SINP-MSU-80 (Scorpion)
Alternate Names
НИИЯФ-МГУ-80 (Скорпион), RS89S
Satellite ID
OTDY-2434-1908-3059-5807
Temporary NORAD ID
98427
Followed NORAD ID
67293
Website
https://spacepi.space/satellites/skorpion/
Country of Origin

Russia

Status
Satellite alive
Operational

Satellite is in orbit and operational


Frequency Misuse

Satellite is reported to be transmitting at an uncoordinated or denied frequency. Details

Image
SINP-MSU-80 (Scorpion)
Mission timeline
Launch Date
2025-12-28T13:18:00+00:00
Description

The small spacecraft "SINP-MSU-80 (Scorpion)" of the Lomonosov Moscow State University Skobeltsyn Institute of Nuclear Physics was developed jointly with NILAKT DOSAAF based on the CubeSat standard in a 16U form factor. February 1, 2026, marks the 80th anniversary (http://sinp.msu.ru/ru/page/26408) of the founding of the Skobeltsyn Institute of Nuclear Physics. The satellite was named in honor of this event.

The primary mission of the SINP-MSU-80 spacecraft is to obtain radiation data in polar sun-synchronous orbits using cosmic radiation detectors developed at SINP MSU in a limited-orientation flight on a small CubeSat platform with a specified onboard electronics configuration. The combined operation of the fast optical telescope, gamma-ray and charged-particle detectors is aimed at a comprehensive study of cosmophysical and astrophysical phenomena, as well as high-altitude atmospheric discharges. Another important objective is to conduct astrobiology research, specifically studying the impact of space factors on biological systems and developing methods for searching for microorganisms on space objects.

Coordinated observations of charged particle and gamma-ray fluxes will allow us to study the mechanisms of magnetospheric dynamics and create a prototype system for assessing space weather conditions. The experimental equipment located on board is an important stage in the development of satellite experiment technologies at the Lomonosov Moscow State University Skobeltsyn Institute of Nuclear Physics, the main objective of which is to develop a dynamic model of the near-Earth radiation environment in various orbits.

Type
Transmitter
Downlink Mode
DOKA
Downlink Frequency
435240000
Baud
9600
IARU Coordination
IARU Uncoordinated
Mode U - AFSK1k2
Type
Transmitter
Downlink Mode
AFSK
Downlink Frequency
435240000
Baud
1200
IARU Coordination
IARU Uncoordinated
Mode U - AFSK1k2
Type
Transmitter
Downlink Mode
AFSK
Downlink Frequency
435340000
Baud
1200
IARU Coordination
IARU Uncoordinated
Type
Transmitter
Downlink Mode
DOKA
Downlink Frequency
435340000
Baud
9600
IARU Coordination
IARU Uncoordinated
Type
Transmitter
Downlink Mode
BPSK
Downlink Frequency
2401000000
IARU Coordination
IARU Uncoordinated
Most Recent Observers (last 24h)
Observer Latest Data
EU1XX-KO33ru 2026-02-01 21:03:07 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
2026-02-02 05:15:30 UTC
TLE Set
1 67293U 25313AX  26032.93133467  .00004159  00000-0  18717-3 0  9996
2 67293 97.4079 109.8425 0012771 101.8578 258.4091 15.21566272 5384
Satellite Suggestion History

Transmitter Suggestion History