GHGSAT-C3, 52737
Orbit data source: Space-Track
GHGSAT-C3, 52737 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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52737 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: 11 hours ago
TLE from 11 hours ago
0 GHGSAT-C3
1 52737U 22057F 26091.52025950 .00009042 00000-0 28302-3 0 9999
2 52737 97.6473 234.4137 0006688 45.0964 315.0819 15.33337729213783Epoch: 2026-04-01T12:29Z
TLE epoch observation values (Epoch: 2026-04-01T12:29:10.420Z)
Latitude
-0.00009°
Longitude
-142.76162°
Altitude
465.723 km
Speed
7.635 km/s
True Right ascension
15h 37m 39s
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
05:08:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
467.396 km
Perigee altitude
458.246 km
Semi-major axis
6,840.958 km
Eccentricity
0.00067
Inclination
97.6473°
RAAN
234.4137°
Arg. of periapsis
45.0964°
True anomaly
315.02775°
Mean anomaly
315.0819°
Eccentric anomaly
315.05483°
Mean motion
3.8359 °/min
Orbital period
93.85 mins
BSTAR
0.00028302
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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-C3 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 | 2026-04-02 08:59:14.867Z | 130.674° SE | 2026-04-02 09:01:14.867Z | 89.433° E | 26.581° | 2026-04-02 09:04:14.867Z | 13.115° NNE |
| 5 mins | 2026-04-02 21:57:14.867Z | 40.681° NE | 2026-04-02 21:59:14.867Z | 100.055° ESE | 31.38° | 2026-04-02 22:02:14.867Z | 167.074° S |
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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