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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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, 0.2 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 SIT-HSE
1 61763U 24199AE 26309.93963655 .00059891 00000-0 62882-3 0 9995
2 61763 97.2706 189.3897 0006311 100.6582 259.5389 15.64150544159656Epoch: 2026-11-05T22:33Z
TLE epoch observation values (Epoch: 2026-11-05T22:33:04.597Z)
Latitude
0.00002°
Longitude
165.95414°
Altitude
379.613 km
Speed
7.682 km/s
True Right ascension
12h 37m 33s
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
10:37:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
376.845 km
Perigee altitude
368.324 km
Semi-major axis
6,750.721 km
Eccentricity
0.00063
Inclination
97.2706°
RAAN
189.3897°
Arg. of periapsis
100.6582°
True anomaly
259.46779°
Mean anomaly
259.5389°
Eccentric anomaly
259.50335°
Mean motion
3.91307 °/min
Orbital period
92 mins
BSTAR
0.00062882
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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
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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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| SIT-HSE is likely not visible in the next few days. |
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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