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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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: 11 hours ago
TLE from 11 hours ago
0 GHGSAT-C8
1 56186U 23054J 25310.28477666 .00019086 00000-0 39931-3 0 9999
2 56186 97.3140 211.6192 0007422 135.8464 224.3379 15.45478909143921Epoch: 2025-11-06T06:50Z
TLE epoch observation values (Epoch: 2025-11-06T06:50:04.703Z)
Latitude
-0°
Longitude
63.35431°
Altitude
436.715 km
Speed
7.648 km/s
True Right ascension
14h 06m 28s
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
14:13:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
431.95 km
Perigee altitude
421.849 km
Semi-major axis
6,805.036 km
Eccentricity
0.00074
Inclination
97.314°
RAAN
211.6192°
Arg. of periapsis
135.8464°
True anomaly
224.2785°
Mean anomaly
224.3379°
Eccentric anomaly
224.3082°
Mean motion
3.86632 °/min
Orbital period
93.11 mins
BSTAR
0.00039931
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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 | 2025-11-07 06:41:54.981Z | 358.331° N | 2025-11-07 06:44:54.981Z | 258.961° W | 35.887° | 2025-11-07 06:46:54.981Z | 212.957° SW |
| 4 mins | 2025-11-07 17:10:54.981Z | 112.316° ESE | 2025-11-07 17:11:54.981Z | 76.503° E | 28.751° | 2025-11-07 17:14:54.981Z | 7.751° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
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