POLYITAN 1, 40042
Orbit data source: Space-Track
POLYITAN 1, 40042 is a payload satellite owned by Kyiv Polytechnic (UA) in SSO that was launched on Thu, 19 Jun 2014 UTC via a DNEPR launch vehicle from the Orenburg, Russia (OREN). 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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40042 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
UA / UKRRelated business
Manufacturer
Kyiv Polytechnic
Mission
Operational Commercial Technology
Bus & Motor
CUBESAT 1U, Unknown motor
Mass
1 kg wet, 1 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.015 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 POLYITAN 1
1 40042U 14033AJ 25308.94623749 .00017648 00000-0 73670-3 0 9995
2 40042 98.1086 310.4285 0007523 194.1245 165.9781 15.23705360619331Epoch: 2025-11-04T22:42Z
TLE epoch observation values (Epoch: 2025-11-04T22:42:34.919Z)
Latitude
0.00001°
Longitude
-74.64297°
Altitude
502.768 km
Speed
7.61 km/s
True Right ascension
20h 41m 42s
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
15:54:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
496.836 km
Perigee altitude
486.5 km
Semi-major axis
6,869.805 km
Eccentricity
0.00075
Inclination
98.1086°
RAAN
310.4285°
Arg. of periapsis
194.1245°
True anomaly
165.99897°
Mean anomaly
165.9781°
Eccentric anomaly
165.98854°
Mean motion
3.81177 °/min
Orbital period
94.44 mins
BSTAR
0.0007367
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Other satellites on launch #33 in the year 2014 (2014-06-19 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.POLYITAN 1 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-11-06 00:03:10.313Z | 154.722° SSE | 2025-11-06 00:06:10.313Z | 93.34° ESE | 41.351° | 2025-11-06 00:09:10.313Z | 356.183° N |
| 5 mins | 2025-11-06 13:07:10.313Z | 18.599° NNE | 2025-11-06 13:09:10.313Z | 166.064° S | 43.191° | 2025-11-06 13:12:10.313Z | 190.362° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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