IONOSFERA-M 04

Satellite information

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Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite IONOSFERA-M 04 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 04.

Object identification

Identified? True

Debris? False

Object name: IONOSFERA-M 04

International designator: 2025-155B

Object number (NORAD): 64877

Object ID (CCSDS): 64877

Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 101.323 minutes

Inclination: 98.5564 deg

SMA: 7199.464 km

Apoapsis: 822.552 km

Periapsis: 820.107 km

RAAN: 191.2285 deg

Eccentricy: 0.0001698

Argument of periapsis: 62.1672 deg

Mean anomaly: 297.9677 deg

Mean motion: 14.21191154 rev/day

Mean motion (dot): 0.00000073 rev/day2

B* drag term: 0.000052912 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, 9:05 p.m. UTC

TLE line 0: 0 IONOSFERA-M 04

TLE line 1: 1 64877U 25155B 25225.87864728 .00000073 00000-0 52912-4 0 9999

TLE line 2: 2 64877 98.5564 191.2285 0001698 62.1672 297.9677 14.21191154 2746

Live tracking on map

Real-time ground track for satellite IONOSFERA-M 04.

In-orbit conjunctions

There are no conjunctions computed for IONOSFERA-M 04, at the moment. Check back to stay up to date, as we update our databases every day.

Go to all conjunctions

Associated 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 04 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.

Launch to space Soyuz 2.1b/Fregat-M | Ionosfera-M 3 & 4
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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