GHGSAT-C4, 52746
Orbit data source: Space-Track
GHGSAT-C4, 52746 is a payload satellite owned by GHG (CA) in SSO that was launched on Wed, 25 May 2022 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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52746 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: 17 hours ago
TLE from 17 hours ago
0 GHGSAT-C4
1 52746U 22057Q 25348.92282806 .00006953 00000-0 23192-3 0 9992
2 52746 97.6262 122.4104 0007451 48.4699 311.7179 15.31382750197314Epoch: 2025-12-14T22:08Z
TLE epoch observation values (Epoch: 2025-12-14T22:08:52.344Z)
Latitude
-0.00009°
Longitude
66.36352°
Altitude
471.39 km
Speed
7.632 km/s
True Right ascension
08h 09m 38s
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
13:18:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
473.748 km
Perigee altitude
463.545 km
Semi-major axis
6,846.783 km
Eccentricity
0.00075
Inclination
97.6262°
RAAN
122.4104°
Arg. of periapsis
48.4699°
True anomaly
311.65413°
Mean anomaly
311.7179°
Eccentric anomaly
311.68602°
Mean motion
3.83101 °/min
Orbital period
93.97 mins
BSTAR
0.00023192
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Other satellites on launch #57 in the year 2022 (2022-05-25 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-C4 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 | 2025-12-15 22:13:17.142Z | 1.442° NNE | 2025-12-15 22:16:17.142Z | 300.736° NW | 37.986° | 2025-12-15 22:19:17.142Z | 211.006° SW |
| 4 mins | 2025-12-16 08:48:17.142Z | 128.88° SE | 2025-12-16 08:49:17.142Z | 94.747° ESE | 34.596° | 2025-12-16 08:52:17.142Z | 4.263° 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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