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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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-C7
1 56209U 23054AH 26049.23476440 .00011258 00000-0 22363-3 0 9993
2 56209 97.3103 316.2786 0010230 104.4969 255.7416 15.47093530159988Epoch: 2026-02-18T05:38Z
TLE epoch observation values (Epoch: 2026-02-18T05:38:03.644Z)
Latitude
-0.00007°
Longitude
83.5601°
Altitude
430.085 km
Speed
7.653 km/s
True Right ascension
21h 05m 06s
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
22:33:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
429.116 km
Perigee altitude
415.203 km
Semi-major axis
6,800.296 km
Eccentricity
0.00102
Inclination
97.3103°
RAAN
316.2786°
Arg. of periapsis
104.4969°
True anomaly
255.62802°
Mean anomaly
255.7416°
Eccentric anomaly
255.68481°
Mean motion
3.87036 °/min
Orbital period
93.01 mins
BSTAR
0.00022363
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-02-19 07:01:10.067Z | 352.214° N | 2026-02-19 07:04:10.067Z | 279.171° WNW | 28.899° | 2026-02-19 07:06:10.067Z | 227.125° WSW |
| 4 mins | 2026-02-19 17:29:10.067Z | 137.842° SSE | 2026-02-19 17:31:10.067Z | 53.008° ENE | 34.858° | 2026-02-19 17:33:10.067Z | 4.928° 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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