IONOSFERA-M 01, 61735
Orbit data source: Space-Track
IONOSFERA-M 01, 61735 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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61735 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: 9 hours ago
TLE from 9 hours ago
0 IONOSFERA-M 01
1 61735U 24199A 25312.85919374 .00000115 00000-0 71115-4 0 9992
2 61735 98.7439 182.9625 0002031 70.4073 289.7324 14.22702303 96378Epoch: 2025-11-08T20:37Z
TLE epoch observation values (Epoch: 2025-11-08T20:37:14.339Z)
Latitude
-0°
Longitude
-174.63001°
Altitude
818.652 km
Speed
7.444 km/s
True Right ascension
12h 11m 51s
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
02:01:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
814.846 km
Perigee altitude
811.924 km
Semi-major axis
7,191.522 km
Eccentricity
0.0002
Inclination
98.7439°
RAAN
182.9625°
Arg. of periapsis
70.4073°
True anomaly
289.71049°
Mean anomaly
289.7324°
Eccentric anomaly
289.72145°
Mean motion
3.55887 °/min
Orbital period
101.16 mins
BSTAR
0.000071115
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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 01 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 | 2025-11-09 15:18:27.536Z | 159.033° S | 2025-11-09 15:22:27.536Z | 106.844° ESE | 44.191° | 2025-11-09 15:27:27.536Z | 349.58° N |
| 8 mins | 2025-11-10 03:36:27.536Z | 43.243° NE | 2025-11-10 03:39:27.536Z | 88.272° E | 27.585° | 2025-11-10 03:44:27.536Z | 158.819° S |
| 7 mins | 2025-11-10 05:16:27.536Z | 344.391° N | 2025-11-10 05:19:27.536Z | 299.165° NW | 27.386° | 2025-11-10 05:23:27.536Z | 237.759° 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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