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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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: 5 hours ago
TLE from 5 hours ago
0 UNISAT 6
1 40012U 14033C 25288.85723837 .00005970 00000-0 67219-3 0 9995
2 40012 97.7583 81.6696 0047461 152.0646 208.3132 14.86188614609843Epoch: 2025-10-15T20:34Z
TLE epoch observation values (Epoch: 2025-10-15T20:34:25.395Z)
Latitude
-0.00009°
Longitude
108.4385°
Altitude
642.131 km
Speed
7.521 km/s
True Right ascension
05h 26m 40s
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
20:09:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
640.035 km
Perigee altitude
573.732 km
Semi-major axis
6,985.021 km
Eccentricity
0.00475
Inclination
97.7583°
RAAN
81.6696°
Arg. of periapsis
152.0646°
True anomaly
208.05659°
Mean anomaly
208.3132°
Eccentric anomaly
208.18476°
Mean motion
3.71785 °/min
Orbital period
96.83 mins
BSTAR
0.00067219
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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 | 2025-10-16 09:38:04.034Z | 129.94° SE | 2025-10-16 09:41:04.034Z | 83.334° E | 26.702° | 2025-10-16 09:45:04.034Z | 10.357° NNE |
| 4 mins | 2025-10-16 11:16:04.034Z | 238.994° WSW | 2025-10-16 11:17:04.034Z | 257.62° W | 20.049° | 2025-10-16 11:20:04.034Z | 309.192° NW |
| 6 mins | 2025-10-16 23:01:04.034Z | 25.137° NE | 2025-10-16 23:03:04.034Z | 79.562° E | 41.88° | 2025-10-16 23:07:04.034Z | 183.275° SSW |
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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