Showing default

IONOSFERA-M 04, 64877

Orbit data source: Space-Track

IONOSFERA-M 04, 64877 is a payload satellite owned by VNIIEM (CIS) in SSO that was launched on Fri, 25 Jul 2025 UTC via a SOYUZ-2-1B launch vehicle from the Vostochny Cosmodrome (VOSTO). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

Loading next visibility...
Identifier
64877, 2025-155B
Orbit
SSO
Country
Flag of CISCIS
Related business
Manufacturer
VNIIEM
Mission
Operational Civil Science
Bus & Motor
IONOSFERA-M, Unknown motor
Mass
430 kg wet, 430 kg dry
Launch date (UTC)
2025-07-25 (6 months ago)
Launch vehicle
SOYUZ-2-1B
Launch site
Vostochny Cosmodrome (VOSTO)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 1 Ant, 14.5 m
Radar Cross Section
2.359 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 6 hours ago

TLE from 6 hours ago
0 IONOSFERA-M 04
1 64877U 25155B   26025.60144021  .00000158  00000-0  91804-4 0  9993
2 64877  98.5845 351.1592 0000427  93.4719 266.6507 14.21455882 26140
Epoch: 2026-01-25T14:26Z
TLE epoch observation values (Epoch: 2026-01-25T14:26:04.434Z)
Latitude
-0.00005°
Longitude
9.73153°
Altitude
823.372 km
Speed
7.441 km/s
True Right ascension
23h 24m 38s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
21:58:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
817.891 km
Perigee altitude
817.277 km
Semi-major axis
7,195.721 km
Eccentricity
0.00004
Inclination
98.5845°
RAAN
351.1592°
Arg. of periapsis
93.4719°
True anomaly
266.64582°
Mean anomaly
266.6507°
Eccentric anomaly
266.64826°
Mean motion
3.55575 °/min
Orbital period
101.24 mins
BSTAR
0.000091804
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|