GHGSAT-C8, 56186
Orbit data source: Space-Track
GHGSAT-C8, 56186 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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56186 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: 9 hours ago
TLE from 9 hours ago
0 GHGSAT-C8
1 56186U 23054J 26133.22448701 .00010623 00000-0 17861-3 0 9991
2 56186 97.3010 41.8740 0004882 161.4957 198.6474 15.51922501173019Epoch: 2026-05-13T05:23Z
TLE epoch observation values (Epoch: 2026-05-13T05:23:15.677Z)
Latitude
-0.00005°
Longitude
90.07111°
Altitude
417.391 km
Speed
7.659 km/s
True Right ascension
02h 47m 29s
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
23:16:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
411.345 km
Perigee altitude
404.719 km
Semi-major axis
6,786.169 km
Eccentricity
0.00049
Inclination
97.301°
RAAN
41.874°
Arg. of periapsis
161.4957°
True anomaly
198.62952°
Mean anomaly
198.6474°
Eccentric anomaly
198.63846°
Mean motion
3.88245 °/min
Orbital period
92.72 mins
BSTAR
0.00017861
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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-C8 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 | 2026-05-13 17:53:51.605Z | 163.586° S | 2026-05-13 17:56:51.605Z | 7.519° NNE | 41.988° | 2026-05-13 17:58:51.605Z | 351.125° N |
| 5 mins | 2026-05-14 06:42:51.605Z | 16.571° NNE | 2026-05-14 06:44:51.605Z | 97.364° ESE | 44.378° | 2026-05-14 06:47:51.605Z | 188.634° 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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