Key statistics
Satellite IONOSFERA-M 03 at a glance.
Uptime
20
Days in orbit
Revolutions
≈ 14.2
Per day
Orbit
SSO
Sun Synchronous Orbit
Inclination
98.6
Latest
Satellite identification and parameters
Extended collection of information and parameters for IONOSFERA-M 03.
Object identification
Identified? True
Debris? False
Object name: IONOSFERA-M 03
International designator: 2025-155A
Object number (NORAD): 64876
Object ID (CCSDS): 64876
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: LARGE
Orbital parameters
Period: 101.259 minutes
Inclination: 98.5564 deg
SMA: 7196.414 km
Apoapsis: 819.932 km
Periapsis: 816.626 km
RAAN: 191.2361 deg
Eccentricy: 0.0002297
Argument of periapsis: 55.9702 deg
Mean anomaly: 304.1694 deg
Mean motion: 14.2209467 rev/day
Mean motion (dot): 0.00000101 rev/day2
B* drag term: 0.000064658 1/REarth
Two-line elements (TLE)
Creation date: Aug. 14, 2025, 2:27 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Aug. 13, 2025, 8:56 p.m. UTC
TLE line 0: 0 IONOSFERA-M 03
TLE line 1: 1 64876U 25155A 25225.87258299 .00000101 00000-0 64658-4 0 9990
TLE line 2: 2 64876 98.5564 191.2361 0002297 55.9702 304.1694 14.22094670 2746
Live tracking on map
Real-time ground track for satellite IONOSFERA-M 03.
In-orbit conjunctions
There are no conjunctions computed for IONOSFERA-M 03, at the moment. Check back to stay up to date, as we update our databases every day.
Go to all conjunctionsAssociated space launch
Ionosfera is a constellation of four ionospheric and magnetospheric research satellites developed by for Roscosmos for the project Ionozond. The satellites will operate on circular sun-synchronous orbits (SSO), at altitude of about 800 km and located in two orbital planes of two satellites each. The following science instruments are carried on the satellites: * SPER/1 Plasma and energy radiation spectrometer * SG/1 Gamma-ray spectrometer * GALS/1 Galactic cosmic ray spectrometer / 1 * LAERTES On-board Ionosonde * NBK/2 Low-frequency wave complex * ESEP Ionospheric plasma energy spectrometer * Ozonometer-TM Ozonometer * MayaK On-board radio transmitters * PES GPS-GLONASS device
IONOSFERA-M 03 was lifted into orbit during the mission ‘Soyuz 2.1b/Fregat-M | Ionosfera-M 3 & 4’, on board a Soyuz 2.1b/Fregat-M space rocket.
The launch took place on July 25, 2025, 5:54 a.m. from Cosmodrome Site 1S.
For more information about the launch, click the button.

Soyuz 2.1b/Fregat-M | Ionosfera-M 3 & 4
Agency: N/A
Status: Launch Successful
Launch date: July 25, 2025, 5:54 a.m. UTC
Rocket: Soyuz 2.1b/Fregat-M
Launch pad: Cosmodrome Site 1S
Location: Vostochny Cosmodrome, Siberia, Russian Federation
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