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: 6 hours ago
TLE from 6 hours ago
0 IONOSFERA-M 02
1 61736U 24199B 26055.77632608 .00000032 00000-0 34164-4 0 9992
2 61736 98.7344 289.9439 0000462 34.1359 325.9848 14.22734784114840Epoch: 2026-02-24T18:37Z
TLE epoch observation values (Epoch: 2026-02-24T18:37:54.573Z)
Latitude
-0.00007°
Longitude
-144.18448°
Altitude
818.761 km
Speed
7.444 km/s
True Right ascension
19h 19m 46s
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
04:21:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
813.607 km
Perigee altitude
812.943 km
Semi-major axis
7,191.412 km
Eccentricity
0.00005
Inclination
98.7344°
RAAN
289.9439°
Arg. of periapsis
34.1359°
True anomaly
325.98184°
Mean anomaly
325.9848°
Eccentric anomaly
325.98332°
Mean motion
3.55895 °/min
Orbital period
101.15 mins
BSTAR
0.000034164
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-02-25 03:39:37.424Z | 35.706° NE | 2026-02-25 03:43:37.424Z | 89.502° E | 28.406° | 2026-02-25 03:48:37.424Z | 160.236° S |
| 7 mins | 2026-02-25 05:20:37.424Z | 343.076° N | 2026-02-25 05:23:37.424Z | 297.508° NW | 26.77° | 2026-02-25 05:27:37.424Z | 238.279° WSW |
| 8 mins | 2026-02-25 15:01:37.424Z | 137.982° SSE | 2026-02-25 15:04:37.424Z | 83.484° E | 37.584° | 2026-02-25 15:09:37.424Z | 358.289° N |
| 6 mins | 2026-02-25 16:42:37.424Z | 232.947° WSW | 2026-02-25 16:45:37.424Z | 273.612° WNW | 18.099° | 2026-02-25 16:48:37.424Z | 309.649° 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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