Showing default

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.

Loading next visibility...
Identifier
40012, 2014-033C
Orbit
SSO
Country
Flag of ITIT
Related business
Manufacturer
GAUSS SrI
Mission
Operational Amateur Technology
Bus & Motor
UNISAT, Unknown motor
Mass
26 kg wet, ~19 kg dry
Launch date (UTC)
2014-06-19 (11 years ago)
Launch vehicle
DNEPR
Launch site
Orenburg, Russia (OREN)
Object type
Payload
Rocket body
Debris
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 & history
Last TLE update: 4 hours ago

TLE from 4 hours ago
0 UNISAT 6
1 40012U 14033C   25308.31342746  .00004236  00000-0  47613-3 0  9995
2 40012  97.7599 100.6599 0047808  89.4321 271.2373 14.86407602612731
Epoch: 2025-11-04T07:31Z
TLE epoch observation values (Epoch: 2025-11-04T07:31:20.132Z)
Latitude
0.00001°
Longitude
-55.97622°
Altitude
611.644 km
Speed
7.554 km/s
True Right ascension
06h 42m 38s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
07:13:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
639.588 km
Perigee altitude
572.806 km
Semi-major axis
6,984.334 km
Eccentricity
0.00478
Inclination
97.7599°
RAAN
100.6599°
Arg. of periapsis
89.4321°
True anomaly
270.68953°
Mean anomaly
271.2373°
Eccentric anomaly
270.96342°
Mean motion
3.7184 °/min
Orbital period
96.82 mins
BSTAR
0.00047613
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|