GHGSAT-C6, 56204
Orbit data source: Space-Track
GHGSAT-C6, 56204 is a payload satellite owned by GHG (CA) in SSO that was launched on Sat, 15 Apr 2023 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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56204 intel report (Beta)
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Edit Public Description
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: 4 hours ago
TLE from 4 hours ago
0 GHGSAT-C6
1 56204U 23054AC 25310.95865308 .00018996 00000-0 39700-3 0 9991
2 56204 97.3172 212.8559 0010507 122.0456 238.1815 15.45481187144048Epoch: 2025-11-06T23:00Z
TLE epoch observation values (Epoch: 2025-11-06T23:00:27.626Z)
Latitude
-0.00001°
Longitude
-178.66871°
Altitude
436.87 km
Speed
7.648 km/s
True Right ascension
14h 11m 25s
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
23:10:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
434.043 km
Perigee altitude
419.743 km
Semi-major axis
6,805.03 km
Eccentricity
0.00105
Inclination
97.3172°
RAAN
212.8559°
Arg. of periapsis
122.0456°
True anomaly
238.07926°
Mean anomaly
238.1815°
Eccentric anomaly
238.13037°
Mean motion
3.86632 °/min
Orbital period
93.11 mins
BSTAR
0.000397
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Other satellites on launch #54 in the year 2023 (2023-04-15 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-C6 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 | 2025-11-07 05:47:43.472Z | 48.926° ENE | 2025-11-07 05:49:43.472Z | 92.698° ESE | 19.91° | 2025-11-07 05:51:43.472Z | 139.552° SSE |
| 5 mins | 2025-11-07 17:47:43.472Z | 180.07° SSW | 2025-11-07 17:49:43.472Z | 275.217° WNW | 42.534° | 2025-11-07 17:52:43.472Z | 342.522° N |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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