SIT-2086, 61764
Orbit data source: Space-Track
SIT-2086, 61764 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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61764 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
Sputniks
Mission
Operational Amateur Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
3 kg wet, 3 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: 11 hours ago
TLE from 11 hours ago
0 SIT-2086
1 61764U 24199AF 25312.87239205 .00027536 00000-0 67166-3 0 9990
2 61764 97.3259 182.0369 0008237 5.9537 354.1806 15.40815128100372Epoch: 2025-11-08T20:56Z
TLE epoch observation values (Epoch: 2025-11-08T20:56:14.673Z)
Latitude
-0°
Longitude
179.67999°
Altitude
441.232 km
Speed
7.65 km/s
True Right ascension
12h 08m 08s
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
04:11:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
446.254 km
Perigee altitude
435.02 km
Semi-major axis
6,818.774 km
Eccentricity
0.00082
Inclination
97.3259°
RAAN
182.0369°
Arg. of periapsis
5.9537°
True anomaly
354.17102°
Mean anomaly
354.1806°
Eccentric anomaly
354.17581°
Mean motion
3.85464 °/min
Orbital period
93.39 mins
BSTAR
0.00067166
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Other satellites on launch #199 in the year 2024 (2024-11-04 UTC)
Did you know?
You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.SIT-2086 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 | 2025-11-09 15:46:21.294Z | 190.392° SSW | 2025-11-09 15:48:21.294Z | 238.978° WSW | 35.046° | 2025-11-09 15:51:21.294Z | 332.91° NNW |
| 4 mins | 2025-11-10 04:41:21.294Z | 333.056° NNW | 2025-11-10 04:42:21.294Z | 294.754° NW | 32.896° | 2025-11-10 04:45:21.294Z | 217.001° SW |
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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