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: 4 hours ago
TLE from 4 hours ago
0 IONOSFERA-M 01
1 61735U 24199A 25342.88932796 .00000161 00000-0 91622-4 0 9997
2 61735 98.7413 212.7670 0001142 27.0748 333.0490 14.22712896100642Epoch: 2025-12-08T21:20Z
TLE epoch observation values (Epoch: 2025-12-08T21:20:37.935Z)
Latitude
0.00003°
Longitude
174.72705°
Altitude
818.377 km
Speed
7.444 km/s
True Right ascension
14h 11m 04s
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
23:37:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
814.17 km
Perigee altitude
812.528 km
Semi-major axis
7,191.486 km
Eccentricity
0.00011
Inclination
98.7413°
RAAN
212.767°
Arg. of periapsis
27.0748°
True anomaly
333.04307°
Mean anomaly
333.049°
Eccentric anomaly
333.04603°
Mean motion
3.5589 °/min
Orbital period
101.15 mins
BSTAR
0.000091622
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-12-09 03:01:53.012Z | 62.508° ENE | 2025-12-09 03:03:53.012Z | 85.913° E | 14.138° | 2025-12-09 03:06:53.012Z | 121.588° SE |
| 9 mins | 2025-12-09 04:40:53.012Z | 4.728° NNE | 2025-12-09 04:44:53.012Z | 274.501° WNW | 42.333° | 2025-12-09 04:49:53.012Z | 205.945° SW |
| 7 mins | 2025-12-09 14:22:53.012Z | 107.54° ESE | 2025-12-09 14:25:53.012Z | 64.914° ENE | 22.224° | 2025-12-09 14:29:53.012Z | 14.095° NNE |
| 8 mins | 2025-12-09 16:01:53.012Z | 196.659° SSW | 2025-12-09 16:05:53.012Z | 269.986° W | 33.924° | 2025-12-09 16:09:53.012Z | 328.933° 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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