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 25360.89325152 .00000059 00000-0 45913-4 0 9998
2 61735 98.7395 230.6321 0000256 1.7716 358.3462 14.22717152103206Epoch: 2025-12-26T21:26Z
TLE epoch observation values (Epoch: 2025-12-26T21:26:16.931Z)
Latitude
-0.00009°
Longitude
173.43416°
Altitude
818.911 km
Speed
7.444 km/s
True Right ascension
15h 22m 31s
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
03:01:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
813.519 km
Perigee altitude
813.151 km
Semi-major axis
7,191.472 km
Eccentricity
0.00003
Inclination
98.7395°
RAAN
230.6321°
Arg. of periapsis
1.7716°
True anomaly
358.34612°
Mean anomaly
358.3462°
Eccentric anomaly
358.34616°
Mean motion
3.55891 °/min
Orbital period
101.15 mins
BSTAR
0.000045913
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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 | 2025-12-27 04:45:33.903Z | 4.6° NNE | 2025-12-27 04:50:33.903Z | 272.64° WNW | 40.407° | 2025-12-27 04:54:33.903Z | 211.752° SW |
| 7 mins | 2025-12-27 14:28:33.903Z | 109.167° ESE | 2025-12-27 14:31:33.903Z | 63.005° ENE | 24.089° | 2025-12-27 14:35:33.903Z | 11.845° NNE |
| 8 mins | 2025-12-27 16:07:33.903Z | 201.226° SSW | 2025-12-27 16:11:33.903Z | 271.629° WNW | 31.492° | 2025-12-27 16:15:33.903Z | 327.188° NNW |
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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