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: 7 hours ago
TLE from 7 hours ago
0 POLYITAN 1
1 40042U 14033AJ 25295.15266747 .00022899 00000-0 97180-3 0 9990
2 40042 98.1094 295.5315 0006354 252.6521 107.4019 15.23093494617235Epoch: 2025-10-22T03:39Z
TLE epoch observation values (Epoch: 2025-10-22T03:39:50.469Z)
Latitude
-0.00002°
Longitude
-150.25916°
Altitude
500.899 km
Speed
7.613 km/s
True Right ascension
19h 42m 07s
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
05:18:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
497.876 km
Perigee altitude
489.143 km
Semi-major axis
6,871.647 km
Eccentricity
0.00064
Inclination
98.1094°
RAAN
295.5315°
Arg. of periapsis
252.6521°
True anomaly
107.47136°
Mean anomaly
107.4019°
Eccentric anomaly
107.43663°
Mean motion
3.81024 °/min
Orbital period
94.48 mins
BSTAR
0.0009718
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-10-22 13:42:22.028Z | 324.539° NNW | 2025-10-22 13:43:22.028Z | 297.607° NW | 25.396° | 2025-10-22 13:46:22.028Z | 232.422° WSW |
| 5 mins | 2025-10-23 00:18:22.028Z | 179.618° S | 2025-10-23 00:20:22.028Z | 283.373° WNW | 42.889° | 2025-10-23 00:23:22.028Z | 341.531° N |
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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