UNISAT 6, 40012
Orbit data source: Space-Track
UNISAT 6, 40012 is a payload satellite owned by GAUSS SrI (IT) 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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40012 intel report (Beta)
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Identifier
Orbit
Country
ITRelated business
Manufacturer
GAUSS SrI
Mission
Operational Amateur Technology
Bus & Motor
UNISAT, Unknown motor
Mass
26 kg wet, ~19 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 4 Pan, 0.4 m
Radar Cross Section
0.238 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 UNISAT 6
1 40012U 14033C 26297.20017347 .00001709 00000-0 18543-3 0 9999
2 40012 97.8044 87.8364 0044533 4.7760 355.3873 14.88787929665352Epoch: 2026-10-24T04:48Z
TLE epoch observation values (Epoch: 2026-10-24T04:48:14.987Z)
Latitude
-0.00003°
Longitude
-16.83582°
Altitude
573.769 km
Speed
7.591 km/s
True Right ascension
05h 51m 20s
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
19:23:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
629.816 km
Perigee altitude
567.676 km
Semi-major axis
6,976.883 km
Eccentricity
0.00445
Inclination
97.8044°
RAAN
87.8364°
Arg. of periapsis
4.776°
True anomaly
355.34603°
Mean anomaly
355.3873°
Eccentric anomaly
355.36669°
Mean motion
3.72435 °/min
Orbital period
96.66 mins
BSTAR
0.00018543
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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.UNISAT 6 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-10-25 09:57:19.473Z | 154.242° SSE | 2026-10-25 10:01:19.473Z | 65.002° ENE | 60.606° | 2026-10-25 10:04:19.473Z | 357.667° N |
| 6 mins | 2026-10-25 23:19:19.473Z | 359.119° N | 2026-10-25 23:22:19.473Z | 251.443° W | 57.418° | 2026-10-25 23:25:19.473Z | 207.335° SW |
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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