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 Amateur 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, 0.087 m
Radar Cross Section
0.015 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 POLYITAN 1
1 40042U 14033AJ 26304.06020119 .00014933 00000-0 40619-3 0 9998
2 40042 98.0808 343.5670 0006968 43.7396 316.4397 15.37631099674446Epoch: 2026-10-31T01:26Z
TLE epoch observation values (Epoch: 2026-10-31T01:26:41.382Z)
Latitude
-0.00011°
Longitude
-77.47676°
Altitude
452.762 km
Speed
7.643 km/s
True Right ascension
22h 54m 16s
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
07:45:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
454.847 km
Perigee altitude
445.331 km
Semi-major axis
6,828.226 km
Eccentricity
0.0007
Inclination
98.0808°
RAAN
343.567°
Arg. of periapsis
43.7396°
True anomaly
316.38464°
Mean anomaly
316.4397°
Eccentric anomaly
316.41217°
Mean motion
3.84664 °/min
Orbital period
93.59 mins
BSTAR
0.00040619
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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 | 2026-10-31 16:03:26.936Z | 355.18° N | 2026-10-31 16:06:26.936Z | 267.89° W | 40.992° | 2026-10-31 16:08:26.936Z | 220.631° SW |
| 5 mins | 2026-11-01 02:34:26.936Z | 147.283° SSE | 2026-11-01 02:36:26.936Z | 91.689° ESE | 53.717° | 2026-11-01 02:39:26.936Z | 358.355° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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