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, 0.1 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 26254.05374823 .00014452 00000-0 41445-3 0 9999
2 40042 98.0899 288.6116 0006186 192.3852 167.7238 15.35994672666764Epoch: 2026-09-11T01:17Z
TLE epoch observation values (Epoch: 2026-09-11T01:17:23.847Z)
Latitude
-0.00007°
Longitude
-80.82037°
Altitude
465.192 km
Speed
7.632 km/s
True Right ascension
19h 14m 26s
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
04:28:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
459.17 km
Perigee altitude
450.716 km
Semi-major axis
6,833.08 km
Eccentricity
0.00062
Inclination
98.0899°
RAAN
288.6116°
Arg. of periapsis
192.3852°
True anomaly
167.73886°
Mean anomaly
167.7238°
Eccentric anomaly
167.73133°
Mean motion
3.84254 °/min
Orbital period
93.69 mins
BSTAR
0.00041445
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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 | 2026-09-11 15:56:11.477Z | 328.056° NNW | 2026-09-11 15:57:11.477Z | 301.713° NW | 27.034° | 2026-09-11 16:00:11.477Z | 232.205° WSW |
| 5 mins | 2026-09-12 02:27:11.477Z | 168.132° S | 2026-09-12 02:29:11.477Z | 339.987° N | 69.487° | 2026-09-12 02:32:11.477Z | 346.639° 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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