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 25322.47104058 .00020837 00000-0 84873-3 0 9997
2 40042 98.1081 325.0480 0009233 148.0532 212.1264 15.24480071621392Epoch: 2025-11-18T11:18Z
TLE epoch observation values (Epoch: 2025-11-18T11:18:17.906Z)
Latitude
-0.0001°
Longitude
97.71675°
Altitude
500.798 km
Speed
7.611 km/s
True Right ascension
21h 40m 11s
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
17:35:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
495.679 km
Perigee altitude
482.998 km
Semi-major axis
6,867.475 km
Eccentricity
0.00092
Inclination
98.1081°
RAAN
325.048°
Arg. of periapsis
148.0532°
True anomaly
212.07019°
Mean anomaly
212.1264°
Eccentric anomaly
212.09829°
Mean motion
3.81371 °/min
Orbital period
94.4 mins
BSTAR
0.00084873
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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 | 2025-11-19 23:40:59.172Z | 120.925° SE | 2025-11-19 23:42:59.172Z | 80.184° E | 23.632° | 2025-11-19 23:45:59.172Z | 15.885° NNE |
| 4 mins | 2025-11-20 12:43:59.172Z | 61.304° ENE | 2025-11-20 12:44:59.172Z | 91.16° ESE | 27.181° | 2025-11-20 12:47:59.172Z | 159.116° 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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