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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46278 intel report (Beta)
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Identifier
Orbit
Country
CARelated 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)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 1.0 m
Radar Cross Section
0.100 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 GHGSAT-C1
1 46278U 20061G 26233.90511720 .00141861 00000-0 85773-3 0 9991
2 46278 97.2064 321.4153 0001741 149.0528 211.0842 15.77198345333814Epoch: 2026-08-21T21:43Z
TLE epoch observation values (Epoch: 2026-08-21T21:43:22.126Z)
Latitude
0.00006°
Longitude
25.34993°
Altitude
342.558 km
Speed
7.703 km/s
True Right ascension
21h 25m 39s
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
15:00:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
336.433 km
Perigee altitude
334.095 km
Semi-major axis
6,713.401 km
Eccentricity
0.00017
Inclination
97.2064°
RAAN
321.4153°
Arg. of periapsis
149.0528°
True anomaly
211.0739°
Mean anomaly
211.0842°
Eccentric anomaly
211.07905°
Mean motion
3.94575 °/min
Orbital period
91.24 mins
BSTAR
0.00085773
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Other satellites on launch #61 in the year 2020 (2020-09-03 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.GHGSAT-C1 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 | 2026-08-24 06:11:24.839Z | 186.968° SSW | 2026-08-24 06:13:24.839Z | 283.97° WNW | 37.25° | 2026-08-24 06:15:24.839Z | 336.322° NNW |
| 4 mins | 2026-08-24 18:47:24.839Z | 13.451° NNE | 2026-08-24 18:49:24.839Z | 184.034° SSW | 41.704° | 2026-08-24 18:51:24.839Z | 191.098° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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