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: 10 hours ago
TLE from 10 hours ago
0 UNISAT 6
1 40012U 14033C 26251.15829096 .00002318 00000-0 25024-3 0 9994
2 40012 97.7989 42.4851 0045292 153.3215 207.0346 14.88595654658505Epoch: 2026-09-08T03:47Z
TLE epoch observation values (Epoch: 2026-09-08T03:47:56.338Z)
Latitude
-0.00008°
Longitude
-1.72835°
Altitude
633.556 km
Speed
7.526 km/s
True Right ascension
02h 49m 56s
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
06:28:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.95 km
Perigee altitude
567.745 km
Semi-major axis
6,977.484 km
Eccentricity
0.00453
Inclination
97.7989°
RAAN
42.4851°
Arg. of periapsis
153.3215°
True anomaly
206.79988°
Mean anomaly
207.0346°
Eccentric anomaly
206.91712°
Mean motion
3.72387 °/min
Orbital period
96.67 mins
BSTAR
0.00025024
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-08 22:07:56.065Z | 50.366° ENE | 2026-09-08 22:10:56.065Z | 100.369° ESE | 18.758° | 2026-09-08 22:12:56.065Z | 133.448° SE |
| 6 mins | 2026-09-08 23:43:56.065Z | 341.823° N | 2026-09-08 23:45:56.065Z | 303.723° NW | 29.816° | 2026-09-08 23:49:56.065Z | 227.77° WSW |
| 6 mins | 2026-09-09 10:34:56.065Z | 192.348° SSW | 2026-09-09 10:37:56.065Z | 273.153° WNW | 48.357° | 2026-09-09 10:40:56.065Z | 332.036° NNW |
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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