IONOSFERA-M 02, 61736
Orbit data source: Space-Track
IONOSFERA-M 02, 61736 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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61736 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: 8 hours ago
TLE from 8 hours ago
0 IONOSFERA-M 02
1 61736U 24199B 25360.92787763 .00000079 00000-0 55039-4 0 9995
2 61736 98.7394 230.5788 0001876 92.2504 267.8889 14.22719408106331Epoch: 2025-12-26T22:16Z
TLE epoch observation values (Epoch: 2025-12-26T22:16:08.627Z)
Latitude
0.00002°
Longitude
160.88132°
Altitude
819.138 km
Speed
7.444 km/s
True Right ascension
15h 22m 18s
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
05:21:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
814.676 km
Perigee altitude
811.978 km
Semi-major axis
7,191.464 km
Eccentricity
0.00019
Inclination
98.7394°
RAAN
230.5788°
Arg. of periapsis
92.2504°
True anomaly
267.86742°
Mean anomaly
267.8889°
Eccentric anomaly
267.87816°
Mean motion
3.55891 °/min
Orbital period
101.15 mins
BSTAR
0.000055039
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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 02 Visibility forecast
Loading observer location...
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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-12-27 15:15:26.309Z | 157.223° SSE | 2025-12-27 15:20:26.309Z | 65.707° ENE | 43.748° | 2025-12-27 15:25:26.309Z | 350.697° N |
| 7 mins | 2025-12-28 03:34:26.309Z | 47.742° ENE | 2025-12-28 03:37:26.309Z | 95.464° ESE | 26.367° | 2025-12-28 03:41:26.309Z | 152.473° SSE |
| 7 mins | 2025-12-28 05:14:26.309Z | 342.929° N | 2025-12-28 05:17:26.309Z | 292.032° WNW | 28.871° | 2025-12-28 05:21:26.309Z | 233.491° WSW |
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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