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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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: 14 hours ago
TLE from 14 hours ago
0 GHGSAT-C6
1 56204U 23054AC 26049.23301722 .00014248 00000-0 26269-3 0 9999
2 56204 97.3144 317.2750 0010191 109.4433 250.7921 15.49184800160012Epoch: 2026-02-18T05:35Z
TLE epoch observation values (Epoch: 2026-02-18T05:35:32.687Z)
Latitude
0.00003°
Longitude
85.1872°
Altitude
424.528 km
Speed
7.655 km/s
True Right ascension
21h 09m 05s
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
22:35:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
422.957 km
Perigee altitude
409.109 km
Semi-major axis
6,794.17 km
Eccentricity
0.00102
Inclination
97.3144°
RAAN
317.275°
Arg. of periapsis
109.4433°
True anomaly
250.68187°
Mean anomaly
250.7921°
Eccentric anomaly
250.73698°
Mean motion
3.8756 °/min
Orbital period
92.89 mins
BSTAR
0.00026269
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-02-19 06:56:41.969Z | 357.958° N | 2026-02-19 06:59:41.969Z | 274.973° WNW | 35.007° | 2026-02-19 07:01:41.969Z | 217.288° SW |
| 4 mins | 2026-02-19 17:23:41.969Z | 128.248° SE | 2026-02-19 17:25:41.969Z | 65.92° ENE | 28.551° | 2026-02-19 17:27:41.969Z | 14.146° NNE |
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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