GHGSAT-C2, 47509
Orbit data source: Space-Track
GHGSAT-C2, 47509 is a payload satellite owned by GHG (CA) in SSO that was launched on Sun, 24 Jan 2021 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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47509 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: 15 hours ago
TLE from 15 hours ago
0 GHGSAT-C2
1 47509U 21006DA 26306.68609999 .00004293 00000-0 11259-3 0 9996
2 47509 97.1981 351.5811 0005969 44.4792 315.6932 15.39177548321145Epoch: 2026-11-02T16:27Z
TLE epoch observation values (Epoch: 2026-11-02T16:27:59.039Z)
Latitude
-0.00004°
Longitude
62.62555°
Altitude
448.747 km
Speed
7.645 km/s
True Right ascension
23h 26m 19s
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
02:52:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
449.545 km
Perigee altitude
441.399 km
Semi-major axis
6,823.609 km
Eccentricity
0.0006
Inclination
97.1981°
RAAN
351.5811°
Arg. of periapsis
44.4792°
True anomaly
315.6454°
Mean anomaly
315.6932°
Eccentric anomaly
315.6693°
Mean motion
3.85054 °/min
Orbital period
93.49 mins
BSTAR
0.00011259
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Other satellites on launch #6 in the year 2021 (2021-01-24 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-C2 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-11-03 16:26:39.798Z | 338.183° N | 2026-11-03 16:28:39.798Z | 266.489° W | 35.551° | 2026-11-03 16:30:39.798Z | 222.885° SW |
| 4 mins | 2026-11-04 02:56:39.798Z | 136.803° SSE | 2026-11-04 02:58:39.798Z | 43.642° NE | 44.814° | 2026-11-04 03:00:39.798Z | 3.345° 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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