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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UNISAT 6 radio frequencies
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Edit Public Description
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, 0.5 m
Radar Cross Section
0.238 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 UNISAT 6
1 40012U 14033C 25258.21872965 .00004200 00000-0 48014-3 0 9996
2 40012 97.7547 51.7912 0046086 253.5472 106.0676 14.85789564605290Epoch: 2025-09-15T05:14Z
TLE epoch observation values (Epoch: 2025-09-15T05:14:58.241Z)
Latitude
-0.00004°
Longitude
-21.378°
Altitude
623.196 km
Speed
7.542 km/s
True Right ascension
03h 27m 09s
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
10:59:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
640.332 km
Perigee altitude
575.938 km
Semi-major axis
6,986.272 km
Eccentricity
0.00461
Inclination
97.7547°
RAAN
51.7912°
Arg. of periapsis
253.5472°
True anomaly
106.57426°
Mean anomaly
106.0676°
Eccentric anomaly
106.32101°
Mean motion
3.71685 °/min
Orbital period
96.86 mins
BSTAR
0.00048014
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-09-15 22:00:58.470Z | 61.591° ENE | 2025-09-15 22:02:58.470Z | 89.87° E | 13.484° | 2025-09-15 22:04:58.470Z | 118.885° SE |
| 6 mins | 2025-09-15 23:36:58.470Z | 349.604° N | 2025-09-15 23:38:58.470Z | 300.816° NW | 36.465° | 2025-09-15 23:42:58.470Z | 214.383° SW |
| 6 mins | 2025-09-16 10:28:58.470Z | 176.869° S | 2025-09-16 10:30:58.470Z | 211.458° SW | 42.827° | 2025-09-16 10:34:58.470Z | 342.733° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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