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: 12 hours ago
TLE from 12 hours ago
0 IONOSFERA-M 01
1 61735U 24199A 25260.25321091 .00000025 00000-0 31064-4 0 9990
2 61735 98.7529 130.7216 0000959 141.6543 218.4703 14.22686151 88895Epoch: 2025-09-17T06:04Z
TLE epoch observation values (Epoch: 2025-09-17T06:04:37.422Z)
Latitude
-0.00005°
Longitude
43.13387°
Altitude
819.74 km
Speed
7.443 km/s
True Right ascension
08h 42m 53s
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
11:21:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
814.129 km
Perigee altitude
812.75 km
Semi-major axis
7,191.577 km
Eccentricity
0.0001
Inclination
98.7529°
RAAN
130.7216°
Arg. of periapsis
141.6543°
True anomaly
218.46346°
Mean anomaly
218.4703°
Eccentric anomaly
218.46688°
Mean motion
3.55883 °/min
Orbital period
101.16 mins
BSTAR
0.000031064
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-09-18 02:57:47.588Z | 67.349° ENE | 2025-09-18 02:59:47.588Z | 91.189° ESE | 13.538° | 2025-09-18 03:01:47.588Z | 114.898° SE |
| 8 mins | 2025-09-18 04:36:47.588Z | 4.881° NNE | 2025-09-18 04:39:47.588Z | 318.292° NNW | 42.398° | 2025-09-18 04:44:47.588Z | 205.338° SW |
| 6 mins | 2025-09-18 14:18:47.588Z | 102.479° ESE | 2025-09-18 14:21:47.588Z | 58.144° ENE | 21.352° | 2025-09-18 14:24:47.588Z | 19.41° NNE |
| 8 mins | 2025-09-18 15:57:47.588Z | 197.716° SSW | 2025-09-18 16:00:47.588Z | 250.831° W | 34.88° | 2025-09-18 16:05:47.588Z | 331.733° 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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