TUSUR GO, 61782
Orbit data source: Space-Track
TUSUR GO, 61782 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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61782 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
Geoskan
Mission
Operational 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, 0.1 m
Radar Cross Section
0.035 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 TUSUR GO
1 61782U 24199AZ 25301.67367395 .00055833 00000-0 11155-2 0 9995
2 61782 97.3257 171.1343 0013232 49.7624 310.4781 15.46538553 98682Epoch: 2025-10-28T16:10Z
TLE epoch observation values (Epoch: 2025-10-28T16:10:05.429Z)
Latitude
-0°
Longitude
-108.6461°
Altitude
424.15 km
Speed
7.66 km/s
True Right ascension
11h 24m 32s
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
01:52:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
432.788 km
Perigee altitude
414.788 km
Semi-major axis
6,801.925 km
Eccentricity
0.00132
Inclination
97.3257°
RAAN
171.1343°
Arg. of periapsis
49.7624°
True anomaly
310.36264°
Mean anomaly
310.4781°
Eccentric anomaly
310.42038°
Mean motion
3.86897 °/min
Orbital period
93.05 mins
BSTAR
0.0011155
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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 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-29 15:35:40.806Z | 176.25° S | 2025-10-29 15:37:40.806Z | 219.91° SW | 42.365° | 2025-10-29 15:40:40.806Z | 342.699° N |
| 4 mins | 2025-10-30 04:27:40.806Z | 355.527° N | 2025-10-30 04:28:40.806Z | 312.107° NW | 41.946° | 2025-10-30 04:31:40.806Z | 201.986° SSW |
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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