SIT-HSE, 61763
Orbit data source: Space-Track
SIT-HSE, 61763 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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61763 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: 14 hours ago
TLE from 14 hours ago
0 SIT-HSE
1 61763U 24199AE 25260.25813629 .00012933 00000-0 34432-3 0 9996
2 61763 97.3380 129.2787 0007795 186.6833 173.4310 15.38300575 95431Epoch: 2025-09-17T06:11Z
TLE epoch observation values (Epoch: 2025-09-17T06:11:42.975Z)
Latitude
0.00002°
Longitude
39.91297°
Altitude
459.541 km
Speed
7.634 km/s
True Right ascension
08h 37m 06s
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
13:10:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
453.394 km
Perigee altitude
442.752 km
Semi-major axis
6,826.21 km
Eccentricity
0.00078
Inclination
97.338°
RAAN
129.2787°
Arg. of periapsis
186.6833°
True anomaly
173.44121°
Mean anomaly
173.431°
Eccentric anomaly
173.43611°
Mean motion
3.84834 °/min
Orbital period
93.55 mins
BSTAR
0.00034432
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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.SIT-HSE 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 | 2025-09-18 04:36:42.507Z | 351.737° N | 2025-09-18 04:38:42.507Z | 308.096° NW | 31.628° | 2025-09-18 04:41:42.507Z | 219.249° SW |
| 5 mins | 2025-09-18 15:07:42.507Z | 138.469° SSE | 2025-09-18 15:09:42.507Z | 58.966° ENE | 36.138° | 2025-09-18 15:12:42.507Z | 359.995° N |
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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