GHGSAT-C7, 56209
Orbit data source: Space-Track
GHGSAT-C7, 56209 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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56209 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-C7
1 56209U 23054AH 25310.97576249 .00015617 00000-0 34186-3 0 9991
2 56209 97.3131 212.2021 0010501 116.8169 243.4155 15.44156297144037Epoch: 2025-11-06T23:25Z
TLE epoch observation values (Epoch: 2025-11-06T23:25:05.879Z)
Latitude
0.00004°
Longitude
174.50124°
Altitude
440.192 km
Speed
7.646 km/s
True Right ascension
14h 08m 48s
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
23:10:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
437.938 km
Perigee altitude
423.638 km
Semi-major axis
6,808.925 km
Eccentricity
0.00105
Inclination
97.3131°
RAAN
212.2021°
Arg. of periapsis
116.8169°
True anomaly
243.30795°
Mean anomaly
243.4155°
Eccentric anomaly
243.36172°
Mean motion
3.86301 °/min
Orbital period
93.19 mins
BSTAR
0.00034186
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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-C7 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-11-07 06:11:41.961Z | 22.238° NNE | 2025-11-07 06:14:41.961Z | 106.349° ESE | 38.929° | 2025-11-07 06:17:41.961Z | 178.658° S |
| 4 mins | 2025-11-07 18:13:41.961Z | 226.609° WSW | 2025-11-07 18:14:41.961Z | 253.561° W | 22.846° | 2025-11-07 18:17:41.961Z | 320.912° NNW |
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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