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: 9 hours ago
TLE from 9 hours ago
0 IONOSFERA-M 01
1 61735U 24199A 26264.25848915 .00000026 00000-0 31309-4 0 9997
2 61735 98.7005 136.3467 0000747 146.2524 213.8702 14.22769117141363Epoch: 2026-09-21T06:12Z
TLE epoch observation values (Epoch: 2026-09-21T06:12:13.462Z)
Latitude
0°
Longitude
43.14971°
Altitude
819.368 km
Speed
7.443 km/s
True Right ascension
09h 05m 23s
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
08:06:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
813.695 km
Perigee altitude
812.62 km
Semi-major axis
7,191.295 km
Eccentricity
0.00007
Inclination
98.7005°
RAAN
136.3467°
Arg. of periapsis
146.2524°
True anomaly
213.86543°
Mean anomaly
213.8702°
Eccentric anomaly
213.86781°
Mean motion
3.55904 °/min
Orbital period
101.15 mins
BSTAR
0.000031309
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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 | 2026-09-21 16:26:06.626Z | 205.425° SW | 2026-09-21 16:31:06.626Z | 273.401° WNW | 27.999° | 2026-09-21 16:35:06.626Z | 322.614° NNW |
| 8 mins | 2026-09-22 04:44:06.626Z | 5.336° NNE | 2026-09-22 04:48:06.626Z | 259.542° W | 66.758° | 2026-09-22 04:52:06.626Z | 205.835° SW |
| 6 mins | 2026-09-22 14:26:06.626Z | 103.866° ESE | 2026-09-22 14:29:06.626Z | 60.757° ENE | 23.056° | 2026-09-22 14:32:06.626Z | 20.982° NNE |
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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