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: 11 hours ago
TLE from 11 hours ago
0 IONOSFERA-M 02
1 61736U 24199B 26264.22224426 .00000030 00000-0 32851-4 0 9998
2 61736 98.7004 136.2207 0001890 66.5775 293.5602 14.22772348144486Epoch: 2026-09-21T05:20Z
TLE epoch observation values (Epoch: 2026-09-21T05:20:01.904Z)
Latitude
0.00004°
Longitude
56.10759°
Altitude
818.367 km
Speed
7.444 km/s
True Right ascension
09h 04m 52s
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
08:59:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
814.506 km
Perigee altitude
811.787 km
Semi-major axis
7,191.284 km
Eccentricity
0.00019
Inclination
98.7004°
RAAN
136.2207°
Arg. of periapsis
66.5775°
True anomaly
293.54035°
Mean anomaly
293.5602°
Eccentric anomaly
293.55027°
Mean motion
3.55905 °/min
Orbital period
101.15 mins
BSTAR
0.000032851
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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 | 2026-09-22 03:51:56.134Z | 32.727° NE | 2026-09-22 03:55:56.134Z | 92.246° ESE | 39.929° | 2026-09-22 04:00:56.134Z | 166.84° S |
| 7 mins | 2026-09-22 05:32:56.134Z | 337.994° N | 2026-09-22 05:35:56.134Z | 293.952° NW | 25.648° | 2026-09-22 05:39:56.134Z | 242.179° WSW |
| 9 mins | 2026-09-22 15:12:56.134Z | 148.913° SSE | 2026-09-22 15:16:56.134Z | 76.092° E | 61.376° | 2026-09-22 15:21:56.134Z | 354.319° N |
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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