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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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: 16 hours ago
TLE from 16 hours ago
0 IONOSFERA-M 02
1 61736U 24199B 26309.93341352 .00000038 00000-0 36461-4 0 9993
2 61736 98.6928 181.3546 0000266 45.8660 314.2540 14.22779494150989Epoch: 2026-11-05T22:24Z
TLE epoch observation values (Epoch: 2026-11-05T22:24:06.928Z)
Latitude
0.00001°
Longitude
160.16547°
Altitude
818.753 km
Speed
7.444 km/s
True Right ascension
12h 05m 25s
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
10:38:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
813.313 km
Perigee altitude
812.931 km
Semi-major axis
7,191.259 km
Eccentricity
0.00003
Inclination
98.6928°
RAAN
181.3546°
Arg. of periapsis
45.866°
True anomaly
314.25182°
Mean anomaly
314.254°
Eccentric anomaly
314.25291°
Mean motion
3.55906 °/min
Orbital period
101.15 mins
BSTAR
0.000036461
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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
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-11-06 15:23:32.360Z | 158.94° S | 2026-11-06 15:28:32.360Z | 36.974° NE | 74.176° | 2026-11-06 15:33:32.360Z | 349.603° N |
| 7 mins | 2026-11-07 03:42:32.360Z | 48.361° ENE | 2026-11-07 03:45:32.360Z | 100° ESE | 31.747° | 2026-11-07 03:49:32.360Z | 155.736° SSE |
| 7 mins | 2026-11-07 05:22:32.360Z | 339.338° N | 2026-11-07 05:25:32.360Z | 287.384° WNW | 31.528° | 2026-11-07 05:29:32.360Z | 234.022° 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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