OBJECT E

Satellite information

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Satellite Type and Status

UNKNOWNIN ORBIT

Key statistics

Satellite OBJECT E at a glance.

Uptime

20

Days in orbit

Revolutions

≈ 15.2

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

97.4

Latest

Satellite identification and parameters

Extended collection of information and parameters for OBJECT E.

Object identification

Identified? True

Debris? False

Object name: OBJECT E

International designator: 2025-155E

Object number (NORAD): 64880

Object ID (CCSDS): 64880

Country: TO BE DETERMINED/UNKNOWN (TBD)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 94.608 minutes

Inclination: 97.4143 deg

SMA: 6877.722 km

Apoapsis: 506.222 km

Periapsis: 492.952 km

RAAN: 190.8769 deg

Eccentricy: 0.0009647

Argument of periapsis: 169.2997 deg

Mean anomaly: 190.8446 deg

Mean motion: 15.22074247 rev/day

Mean motion (dot): 0.00008937 rev/day2

B* drag term: 0.00039297 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, 9:37 p.m. UTC

TLE line 0: 0 OBJECT E

TLE line 1: 1 64880U 25155E 25225.90136260 .00008937 00000-0 39297-3 0 9997

TLE line 2: 2 64880 97.4143 190.8769 0009647 169.2997 190.8446 15.22074247 33894

Live tracking on map

Real-time ground track for satellite OBJECT E.

In-orbit conjunctions

There are no conjunctions computed for OBJECT E, 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

OBJECT E 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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