GHGSAT-C2, 47509
Orbit data source: Space-Track
GHGSAT-C2, 47509 is a payload satellite owned by GHG (CA) in SSO that was launched on Sun, 24 Jan 2021 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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47509 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: 11 hours ago
TLE from 11 hours ago
0 GHGSAT-C2
1 47509U 21006DA 26078.71102950 .00005568 00000-0 15767-3 0 9995
2 47509 97.2268 127.5152 0006811 121.8585 238.3323 15.36662082286100Epoch: 2026-03-19T17:03Z
TLE epoch observation values (Epoch: 2026-03-19T17:03:52.948Z)
Latitude
-0.00008°
Longitude
54.28806°
Altitude
461.553 km
Speed
7.634 km/s
True Right ascension
08h 30m 03s
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
09:06:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
457.577 km
Perigee altitude
448.271 km
Semi-major axis
6,831.061 km
Eccentricity
0.00068
Inclination
97.2268°
RAAN
127.5152°
Arg. of periapsis
121.8585°
True anomaly
238.2659°
Mean anomaly
238.3323°
Eccentric anomaly
238.2991°
Mean motion
3.84424 °/min
Orbital period
93.65 mins
BSTAR
0.00015767
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Other satellites on launch #6 in the year 2021 (2021-01-24 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-C2 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 | 2026-03-20 15:31:16.597Z | 45.36° ENE | 2026-03-20 15:33:16.597Z | 97.287° ESE | 26.033° | 2026-03-20 15:35:16.597Z | 148.981° SSE |
| 5 mins | 2026-03-21 03:35:16.597Z | 198.625° SSW | 2026-03-21 03:37:16.597Z | 270.669° WNW | 34.732° | 2026-03-21 03:40:16.597Z | 334.528° NNW |
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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