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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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: 21 hours ago
TLE from 21 hours ago
0 GHGSAT-C4
1 52746U 22057Q 26172.56387010 .00005455 00000-0 16627-3 0 9992
2 52746 97.6531 317.2108 0007677 92.3441 267.8681 15.34386787226212Epoch: 2026-06-21T13:31Z
TLE epoch observation values (Epoch: 2026-06-21T13:31:58.376Z)
Latitude
0.00004°
Longitude
-155.54477°
Altitude
466.045 km
Speed
7.633 km/s
True Right ascension
21h 08m 50s
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
21:54:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
464.949 km
Perigee altitude
454.451 km
Semi-major axis
6,837.837 km
Eccentricity
0.00077
Inclination
97.6531°
RAAN
317.2108°
Arg. of periapsis
92.3441°
True anomaly
267.78019°
Mean anomaly
267.8681°
Eccentric anomaly
267.82415°
Mean motion
3.83853 °/min
Orbital period
93.79 mins
BSTAR
0.00016627
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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 | 2026-06-22 22:57:09.682Z | 355.037° N | 2026-06-22 23:00:09.682Z | 283.816° WNW | 32.455° | 2026-06-22 23:03:09.682Z | 217.388° SW |
| 5 mins | 2026-06-23 09:30:09.682Z | 146.675° SSE | 2026-06-23 09:32:09.682Z | 64.631° ENE | 40.015° | 2026-06-23 09:35:09.682Z | 356.852° N |
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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