POLYTECH UNIVERSE-4, 61747
Orbit data source: Space-Track
POLYTECH UNIVERSE-4, 61747 is a payload satellite owned by Polytech (CIS) 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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61747 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
Manufacturer
STTs
Mission
Operational Amateur Science
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
5.07 kg wet, 5.07 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: 17 hours ago
TLE from 17 hours ago
0 POLYTECH UNIVERSE-4
1 61747U 24199N 26309.94249370 .00021576 00000-0 37859-3 0 9994
2 61747 97.2756 184.2035 0009516 114.5007 245.7239 15.50514028159294Epoch: 2026-11-05T22:37Z
TLE epoch observation values (Epoch: 2026-11-05T22:37:11.455Z)
Latitude
0.00004°
Longitude
159.73655°
Altitude
421.023 km
Speed
7.657 km/s
True Right ascension
12h 16m 48s
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
11:46:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
418.606 km
Perigee altitude
405.682 km
Semi-major axis
6,790.281 km
Eccentricity
0.00095
Inclination
97.2756°
RAAN
184.2035°
Arg. of periapsis
114.5007°
True anomaly
245.62455°
Mean anomaly
245.7239°
Eccentric anomaly
245.67422°
Mean motion
3.87893 °/min
Orbital period
92.81 mins
BSTAR
0.00037859
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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.POLYTECH UNIVERSE-4 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 | 2026-11-06 15:47:15.421Z | 164.333° S | 2026-11-06 15:50:15.421Z | 2.915° NNE | 63.511° | 2026-11-06 15:52:15.421Z | 350.55° N |
| 4 mins | 2026-11-07 04:37:15.421Z | 15.231° NNE | 2026-11-07 04:39:15.421Z | 173.829° S | 69.068° | 2026-11-07 04:41:15.421Z | 189.67° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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