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GHGSAT-C1, 46278

Orbit data source: Space-Track

GHGSAT-C1, 46278 is a payload satellite owned by GHG (CA) in SSO that was launched on Thu, 03 Sep 2020 UTC via a VEGA launch vehicle from the French Guiana (FRGUI). 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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Identifier
46278, 2020-061G
Orbit
SSO
Country
Flag of CACA
Related business
Manufacturer
UTIAS-SFL
Mission
Operational Commercial Earth Obs Sci
Bus & Motor
NEMO-V1, Unknown motor
Mass
15 kg wet, 15 kg dry
Launch date (UTC)
2020-09-03 (5 years ago)
Launch vehicle
VEGA
Launch site
French Guiana (FRGUI)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 1.0 m
Radar Cross Section
0.100 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 9 hours ago

TLE from 9 hours ago
0 GHGSAT-C1
1 46278U 20061G   25345.29687111  .00070463  00000-0  90558-3 0  9990
2 46278  97.2314  60.9009 0002295  45.4406 314.7037 15.58864973294095
Epoch: 2025-12-11T07:07Z
TLE epoch observation values (Epoch: 2025-12-11T07:07:29.663Z)
Latitude
-0.00012°
Longitude
-126.22755°
Altitude
392.996 km
Speed
7.675 km/s
True Right ascension
04h 03m 36s
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
14:09:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
389.4 km
Perigee altitude
386.295 km
Semi-major axis
6,765.985 km
Eccentricity
0.00023
Inclination
97.2314°
RAAN
60.9009°
Arg. of periapsis
45.4406°
True anomaly
314.685°
Mean anomaly
314.7037°
Eccentric anomaly
314.69435°
Mean motion
3.89984 °/min
Orbital period
92.31 mins
BSTAR
0.00090558
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Computing Atmospheric mass density...

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