POLYTECH UNIVERSE-5, 61745
Orbit data source: Space-Track
POLYTECH UNIVERSE-5, 61745 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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61745 intel report (Beta)
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Edit Public Description
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, 0.1 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 POLYTECH UNIVERSE-5
1 61745U 24199L 25295.16238926 .00033744 00000-0 81528-3 0 9996
2 61745 97.3296 164.0890 0010776 69.5339 290.7064 15.41037866100791Epoch: 2025-10-22T03:53Z
TLE epoch observation values (Epoch: 2025-10-22T03:53:50.432Z)
Latitude
0.00004°
Longitude
74.78891°
Altitude
443.573 km
Speed
7.647 km/s
True Right ascension
10h 56m 21s
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
07:18:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
447.327 km
Perigee altitude
432.632 km
Semi-major axis
6,818.117 km
Eccentricity
0.00108
Inclination
97.3296°
RAAN
164.089°
Arg. of periapsis
69.5339°
True anomaly
290.59084°
Mean anomaly
290.7064°
Eccentric anomaly
290.64862°
Mean motion
3.8552 °/min
Orbital period
93.38 mins
BSTAR
0.00081528
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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-5 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 | 2025-10-22 14:57:02.025Z | 128.969° SE | 2025-10-22 14:59:02.025Z | 78.045° E | 27.491° | 2025-10-22 15:02:02.025Z | 9.453° NNE |
| 4 mins | 2025-10-23 03:51:02.025Z | 43.23° NE | 2025-10-23 03:53:02.025Z | 109.34° ESE | 30.126° | 2025-10-23 03:55:02.025Z | 159.818° S |
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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