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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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: 5 hours ago
TLE from 5 hours ago
0 IONOSFERA-M 01
1 61735U 24199A 26127.89692338 .00000036 00000-0 35783-4 0 9992
2 61735 98.7225 1.4840 0000188 134.5192 225.6001 14.22746750121970Epoch: 2026-05-07T21:31Z
TLE epoch observation values (Epoch: 2026-05-07T21:31:34.180Z)
Latitude
-0.00003°
Longitude
172.85511°
Altitude
819.091 km
Speed
7.444 km/s
True Right ascension
00h 05m 56s
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
10:21:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
813.369 km
Perigee altitude
813.099 km
Semi-major axis
7,191.371 km
Eccentricity
0.00002
Inclination
98.7225°
RAAN
1.484°
Arg. of periapsis
134.5192°
True anomaly
225.59856°
Mean anomaly
225.6001°
Eccentric anomaly
225.59933°
Mean motion
3.55898 °/min
Orbital period
101.15 mins
BSTAR
0.000035783
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-05-08 03:11:50.286Z | 52.02° ENE | 2026-05-08 03:14:50.286Z | 87.073° E | 16.55° | 2026-05-08 03:17:50.286Z | 125.448° SE |
| 8 mins | 2026-05-08 04:51:50.286Z | 0.038° NNE | 2026-05-08 04:55:50.286Z | 273.001° WNW | 39.453° | 2026-05-08 04:59:50.286Z | 213.463° SW |
| 7 mins | 2026-05-08 14:33:50.286Z | 110.011° ESE | 2026-05-08 14:36:50.286Z | 62.204° ENE | 24.904° | 2026-05-08 14:40:50.286Z | 10.924° NNE |
| 8 mins | 2026-05-08 16:12:50.286Z | 203.138° SW | 2026-05-08 16:16:50.286Z | 272.107° WNW | 30.452° | 2026-05-08 16:20:50.286Z | 326.467° NNW |
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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