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: 1 day ago
TLE from 1 day ago
0 POLYITAN 1
1 40042U 14033AJ 25338.28637659 .00039974 00000-0 15879-2 0 9992
2 40042 98.1074 342.1604 0010383 102.8464 257.3933 15.25161140623808Epoch: 2025-12-04T06:52Z
TLE epoch observation values (Epoch: 2025-12-04T06:52:22.937Z)
Latitude
0.00004°
Longitude
165.71983°
Altitude
494.942 km
Speed
7.616 km/s
True Right ascension
22h 48m 38s
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
09:05:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
494.42 km
Perigee altitude
480.164 km
Semi-major axis
6,865.429 km
Eccentricity
0.00104
Inclination
98.1074°
RAAN
342.1604°
Arg. of periapsis
102.8464°
True anomaly
257.27722°
Mean anomaly
257.3933°
Eccentric anomaly
257.33526°
Mean motion
3.81541 °/min
Orbital period
94.35 mins
BSTAR
0.0015879
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Other satellites on launch #33 in the year 2014 (2014-06-19 UTC)
Did you know?
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 | 2025-12-05 13:20:29.206Z | 12.553° NNE | 2025-12-05 13:23:29.206Z | 10.928° NNE | 42.828° | 2025-12-05 13:26:29.206Z | 194.231° SSW |
| 5 mins | 2025-12-05 23:57:29.206Z | 127.915° SE | 2025-12-05 23:59:29.206Z | 76.824° E | 29.527° | 2025-12-06 00:02:29.206Z | 8.388° 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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