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: 4 hours ago
TLE from 4 hours ago
0 IONOSFERA-M 02
1 61736U 24199B 25302.55560194 .00000075 00000-0 53280-4 0 9999
2 61736 98.7450 172.6470 0000243 50.6867 309.4332 14.22701048 98039Epoch: 2025-10-29T13:20Z
TLE epoch observation values (Epoch: 2025-10-29T13:20:04.007Z)
Latitude
-0.00007°
Longitude
-65.49674°
Altitude
819.038 km
Speed
7.444 km/s
True Right ascension
11h 30m 35s
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
13:05:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
813.564 km
Perigee altitude
813.214 km
Semi-major axis
7,191.526 km
Eccentricity
0.00002
Inclination
98.745°
RAAN
172.647°
Arg. of periapsis
50.6867°
True anomaly
309.43105°
Mean anomaly
309.4332°
Eccentric anomaly
309.43212°
Mean motion
3.55887 °/min
Orbital period
101.16 mins
BSTAR
0.00005328
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-10-30 03:26:31.145Z | 45.776° ENE | 2025-10-30 03:29:31.145Z | 86.264° E | 23.64° | 2025-10-30 03:33:31.145Z | 145.082° SSE |
| 8 mins | 2025-10-30 05:06:31.145Z | 349.72° N | 2025-10-30 05:10:31.145Z | 278.857° WNW | 30.949° | 2025-10-30 05:14:31.145Z | 226.909° WSW |
| 8 mins | 2025-10-30 14:47:31.145Z | 131.03° SE | 2025-10-30 14:51:31.145Z | 58.231° ENE | 32.834° | 2025-10-30 14:55:31.145Z | 3.594° NNE |
| 6 mins | 2025-10-30 16:28:31.145Z | 225.194° WSW | 2025-10-30 16:31:31.145Z | 270.374° WNW | 22.196° | 2025-10-30 16:34:31.145Z | 311.168° NW |
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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