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: 6 hours ago
TLE from 6 hours ago
0 IONOSFERA-M 01
1 61735U 24199A 26055.81213124 .00000028 00000-0 32181-4 0 9996
2 61735 98.7345 290.0677 0002074 94.8071 265.3343 14.22732472111725Epoch: 2026-02-24T19:29Z
TLE epoch observation values (Epoch: 2026-02-24T19:29:28.139Z)
Latitude
-0.00008°
Longitude
-156.98583°
Altitude
819.166 km
Speed
7.444 km/s
True Right ascension
19h 20m 16s
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
04:20:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
814.774 km
Perigee altitude
811.791 km
Semi-major axis
7,191.42 km
Eccentricity
0.00021
Inclination
98.7345°
RAAN
290.0677°
Arg. of periapsis
94.8071°
True anomaly
265.31061°
Mean anomaly
265.3343°
Eccentric anomaly
265.32246°
Mean motion
3.55894 °/min
Orbital period
101.15 mins
BSTAR
0.000032181
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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 | 2026-02-25 04:31:15.790Z | 11.545° NNE | 2026-02-25 04:35:15.790Z | 227.754° WSW | 44.504° | 2026-02-25 04:40:15.790Z | 197.608° SSW |
| 5 mins | 2026-02-25 14:14:15.790Z | 90.448° ESE | 2026-02-25 14:16:15.790Z | 62.803° ENE | 18.251° | 2026-02-25 14:19:15.790Z | 24.661° NE |
| 8 mins | 2026-02-25 15:52:15.790Z | 187.565° SSW | 2026-02-25 15:56:15.790Z | 280.104° WNW | 38.717° | 2026-02-25 16:00:15.790Z | 335.048° 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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