IONOSFERA-M 01, 61735
Orbit data source: Space-Track
IONOSFERA-M 01, 61735 is a payload satellite owned by VNIIEM (CIS) in SSO that was launched on Mon, 04 Nov 2024 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.
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61735 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
Manufacturer
VNIIEM
Mission
Operational Civil Science
Bus & Motor
IONOSFERA-M, Unknown motor
Mass
430 kg wet, 430 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Ant, 5.0 m
Radar Cross Section
2.359 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 IONOSFERA-M 01
1 61735U 24199A 26307.78970376 .00000014 00000-0 25653-4 0 9992
2 61735 98.6932 179.3292 0002074 89.8075 270.3341 14.22775529147550Epoch: 2026-11-03T18:57Z
TLE epoch observation values (Epoch: 2026-11-03T18:57:10.404Z)
Latitude
-0.00002°
Longitude
-148.01147°
Altitude
818.892 km
Speed
7.444 km/s
True Right ascension
11h 57m 19s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
23:08:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
814.627 km
Perigee altitude
811.644 km
Semi-major axis
7,191.273 km
Eccentricity
0.00021
Inclination
98.6932°
RAAN
179.3292°
Arg. of periapsis
89.8075°
True anomaly
270.31033°
Mean anomaly
270.3341°
Eccentric anomaly
270.32222°
Mean motion
3.55905 °/min
Orbital period
101.15 mins
BSTAR
0.000025653
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Other satellites on launch #199 in the year 2024 (2024-11-04 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.IONOSFERA-M 01 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-11-04 03:58:04.962Z | 26.462° NE | 2026-11-04 04:03:04.962Z | 98.986° ESE | 45.913° | 2026-11-04 04:08:04.962Z | 172.029° S |
| 6 mins | 2026-11-04 05:40:04.962Z | 333.524° NNW | 2026-11-04 05:43:04.962Z | 290.175° WNW | 22.613° | 2026-11-04 05:46:04.962Z | 251.354° W |
| 9 mins | 2026-11-04 15:20:04.962Z | 153.622° SSE | 2026-11-04 15:24:04.962Z | 57.362° ENE | 69.374° | 2026-11-04 15:29:04.962Z | 351.5° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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