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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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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 3 days ago
TLE from 3 days ago
0 POLYITAN 1
1 40042U 14033AJ 26170.59745425 .00015082 00000-0 47014-3 0 9993
2 40042 98.0942 197.0866 0008761 134.5443 225.6514 15.33326342653963Epoch: 2026-06-19T14:20Z
TLE epoch observation values (Epoch: 2026-06-19T14:20:20.047Z)
Latitude
-0.00003°
Longitude
74.17893°
Altitude
473.179 km
Speed
7.627 km/s
True Right ascension
13h 08m 20s
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
23:26:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
468.869 km
Perigee altitude
456.882 km
Semi-major axis
6,841.012 km
Eccentricity
0.00088
Inclination
98.0942°
RAAN
197.0866°
Arg. of periapsis
134.5443°
True anomaly
225.57966°
Mean anomaly
225.6514°
Eccentric anomaly
225.61553°
Mean motion
3.83586 °/min
Orbital period
93.85 mins
BSTAR
0.00047014
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-22 14:56:39.474Z | 1.097° NNE | 2026-06-22 14:59:39.474Z | 248.98° W | 37.857° | 2026-06-22 15:01:39.474Z | 210.07° SW |
| 5 mins | 2026-06-23 01:29:39.474Z | 135.576° SSE | 2026-06-23 01:31:39.474Z | 65.536° ENE | 35.05° | 2026-06-23 01:34:39.474Z | 1.015° NNE |
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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