TUSUR GO, 61782 (Decayed)
Orbit data source: Space-Track
TUSUR GO, 61782 was a Commonwealth of Independent States-origin payload satellite in LEO 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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61782 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
Manufacturer
Geoskan
Mission
Decayed Amateur Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
5 kg wet, 5 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 6 months ago
TLE from 6 months ago
0 TUSUR GO
1 61782U 24199AZ 26127.41131630 .14715321 25589-5 30718-3 0 9996
2 61782 97.2709 9.2305 0010121 240.0380 119.9919 16.46273630128537Epoch: 2026-05-07T09:52Z
TLE epoch observation values (Epoch: 2026-05-07T09:52:17.728Z)
Latitude
-0°
Longitude
-4.10121°
Altitude
155.738 km
Speed
7.811 km/s
True Right ascension
00h 36m 55s
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
00:17:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
152.564 km
Perigee altitude
139.357 km
Semi-major axis
6,524.097 km
Eccentricity
0.00101
Inclination
97.2709°
RAAN
9.2305°
Arg. of periapsis
240.038°
True anomaly
120.09228°
Mean anomaly
119.9919°
Eccentric anomaly
120.0421°
Mean motion
4.11872 °/min
Orbital period
87.41 mins
BSTAR
0.00030718
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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.TUSUR GO Visibility
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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. |
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| This satellite is decayed. |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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