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: 14 hours ago
TLE from 14 hours ago
0 GHGSAT-C6
1 56204U 23054AC 25310.24642808 .00018410 00000-0 38527-3 0 9998
2 56204 97.3173 212.1379 0010411 124.0225 236.2014 15.45449823143930Epoch: 2025-11-06T05:54Z
TLE epoch observation values (Epoch: 2025-11-06T05:54:51.386Z)
Latitude
-0.00004°
Longitude
77.7163°
Altitude
437.133 km
Speed
7.647 km/s
True Right ascension
14h 08m 33s
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
16:16:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
434.07 km
Perigee altitude
419.9 km
Semi-major axis
6,805.122 km
Eccentricity
0.00104
Inclination
97.3173°
RAAN
212.1379°
Arg. of periapsis
124.0225°
True anomaly
236.10233°
Mean anomaly
236.2014°
Eccentric anomaly
236.15186°
Mean motion
3.86624 °/min
Orbital period
93.11 mins
BSTAR
0.00038527
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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 05:48:14.672Z | 57.054° ENE | 2025-11-07 05:50:14.672Z | 107.314° ESE | 19.529° | 2025-11-07 05:52:14.672Z | 146.601° SSE |
| 4 mins | 2025-11-07 17:48:14.672Z | 184.283° SSW | 2025-11-07 17:49:14.672Z | 214.553° SW | 40.803° | 2025-11-07 17:52:14.672Z | 341.12° 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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