GHGSAT-C13, 64548
Orbit data source: Space-Track
GHGSAT-C13, 64548 is a payload satellite owned by GHG (CA) in SSO that was launched on Mon, 23 Jun 2025 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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64548 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: 7 hours ago
TLE from 7 hours ago
0 GHGSAT-C13
1 64548U 25135W 26225.14401935 .00002688 00000-0 12202-3 0 9991
2 64548 97.4825 340.1438 0000585 104.8251 255.3050 15.21666557 63515Epoch: 2026-08-13T03:27Z
TLE epoch observation values (Epoch: 2026-08-13T03:27:23.271Z)
Latitude
-0.00001°
Longitude
-33.29098°
Altitude
504.006 km
Speed
7.612 km/s
True Right ascension
22h 40m 34s
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
00:32:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
498.183 km
Perigee altitude
497.378 km
Semi-major axis
6,875.917 km
Eccentricity
0.00006
Inclination
97.4825°
RAAN
340.1438°
Arg. of periapsis
104.8251°
True anomaly
255.29852°
Mean anomaly
255.305°
Eccentric anomaly
255.30176°
Mean motion
3.80669 °/min
Orbital period
94.57 mins
BSTAR
0.00012202
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Other satellites on launch #135 in the year 2025 (2025-06-23 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-C13 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 | 2026-08-13 19:48:44.404Z | 46.463° ENE | 2026-08-13 19:51:44.404Z | 103.008° ESE | 19.023° | 2026-08-13 19:53:44.404Z | 139.643° SSE |
| 4 mins | 2026-08-13 21:23:44.404Z | 321.449° NNW | 2026-08-13 21:24:44.404Z | 298.804° NW | 21.042° | 2026-08-13 21:27:44.404Z | 239.326° WSW |
| 6 mins | 2026-08-14 07:59:44.404Z | 182.681° SSW | 2026-08-14 08:02:44.404Z | 293.526° NW | 39.182° | 2026-08-14 08:05:44.404Z | 339.758° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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