RTU MIREA 1, 61785
Orbit data source: Space-Track
RTU MIREA 1, 61785 is a Commonwealth of Independent States-origin payload satellite 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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61785 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
MIREA
Mission
Operational Amateur Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
4 kg wet, 4 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.035 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 3 hours ago
TLE from 3 hours ago
0 RTU MIREA 1
1 61785U 24199BC 25302.58037347 .00033697 00000-0 82813-3 0 9994
2 61785 97.3278 170.8808 0014520 49.1194 311.1307 15.40470649 98741Epoch: 2025-10-29T13:55Z
TLE epoch observation values (Epoch: 2025-10-29T13:55:44.267Z)
Latitude
-0.00013°
Longitude
-76.2051°
Altitude
441.33 km
Speed
7.651 km/s
True Right ascension
11h 23m 31s
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
12:58:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
451.557 km
Perigee altitude
431.752 km
Semi-major axis
6,819.791 km
Eccentricity
0.00145
Inclination
97.3278°
RAAN
170.8808°
Arg. of periapsis
49.1194°
True anomaly
311.00523°
Mean anomaly
311.1307°
Eccentric anomaly
311.06798°
Mean motion
3.85378 °/min
Orbital period
93.41 mins
BSTAR
0.00082813
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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.RTU MIREA 1 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 | 2025-10-30 04:30:43.403Z | 358.237° N | 2025-10-30 04:33:43.403Z | 273.984° WNW | 36.349° | 2025-10-30 04:36:43.403Z | 210.352° SW |
| 4 mins | 2025-10-30 15:01:43.403Z | 122.504° SE | 2025-10-30 15:02:43.403Z | 88.763° E | 31.001° | 2025-10-30 15:05:43.403Z | 7.067° NNE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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