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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Edit Public Description
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: 6 hours ago
TLE from 6 hours ago
0 IONOSFERA-M 01
1 61735U 24199A 25294.85507419 .00000115 00000-0 71149-4 0 9991
2 61735 98.7456 165.0887 0002059 95.5605 264.5807 14.22696999 93814Epoch: 2025-10-21T20:31Z
TLE epoch observation values (Epoch: 2025-10-21T20:31:18.410Z)
Latitude
-0.00007°
Longitude
-173.27505°
Altitude
819.303 km
Speed
7.443 km/s
True Right ascension
11h 00m 21s
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
21:51:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
814.884 km
Perigee altitude
811.922 km
Semi-major axis
7,191.54 km
Eccentricity
0.00021
Inclination
98.7456°
RAAN
165.0887°
Arg. of periapsis
95.5605°
True anomaly
264.55721°
Mean anomaly
264.5807°
Eccentric anomaly
264.56896°
Mean motion
3.55886 °/min
Orbital period
101.16 mins
BSTAR
0.000071149
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-10-22 03:51:26.932Z | 28.755° NE | 2025-10-22 03:56:26.932Z | 115.331° SE | 34.837° | 2025-10-22 04:00:26.932Z | 169.716° S |
| 6 mins | 2025-10-22 05:33:26.932Z | 328.293° NNW | 2025-10-22 05:35:26.932Z | 298.708° NW | 21.187° | 2025-10-22 05:39:26.932Z | 247.137° WSW |
| 8 mins | 2025-10-22 15:13:26.932Z | 152.562° SSE | 2025-10-22 15:16:26.932Z | 105.179° ESE | 42.652° | 2025-10-22 15:21:26.932Z | 352.159° 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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