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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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: 16 hours ago
TLE from 16 hours ago
0 GHGSAT-C13
1 64548U 25135W 25269.25125594 .00006611 00000-0 32316-3 0 9992
2 64548 97.4585 22.3973 0000920 31.9834 328.1456 15.18561586 14765Epoch: 2025-09-26T06:01Z
TLE epoch observation values (Epoch: 2025-09-26T06:01:48.513Z)
Latitude
0°
Longitude
-73.35555°
Altitude
512.736 km
Speed
7.608 km/s
True Right ascension
01h 29m 35s
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
15:13:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
507.79 km
Perigee altitude
506.524 km
Semi-major axis
6,885.294 km
Eccentricity
0.00009
Inclination
97.4585°
RAAN
22.3973°
Arg. of periapsis
31.9834°
True anomaly
328.14004°
Mean anomaly
328.1456°
Eccentric anomaly
328.14282°
Mean motion
3.79891 °/min
Orbital period
94.76 mins
BSTAR
0.00032316
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-09-27 07:28:05.627Z | 151.523° SSE | 2025-09-27 07:31:05.627Z | 46.696° ENE | 39.719° | 2025-09-27 07:34:05.627Z | 356.579° N |
| 5 mins | 2025-09-27 20:34:05.627Z | 9.535° NNE | 2025-09-27 20:36:05.627Z | 212.916° SW | 44.163° | 2025-09-27 20:39:05.627Z | 194.952° SSW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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