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: 7 hours ago
TLE from 7 hours ago
0 GHGSAT-C13
1 64548U 25135W 25328.47578105 .00004033 00000-0 19457-3 0 9999
2 64548 97.4636 80.8671 0002707 99.1756 260.9785 15.19250041 23759Epoch: 2025-11-24T11:25Z
TLE epoch observation values (Epoch: 2025-11-24T11:25:07.482Z)
Latitude
-0.00003°
Longitude
-154.08928°
Altitude
511.486 km
Speed
7.608 km/s
True Right ascension
05h 23m 28s
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
15:53:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
506.938 km
Perigee altitude
503.212 km
Semi-major axis
6,883.212 km
Eccentricity
0.00027
Inclination
97.4636°
RAAN
80.8671°
Arg. of periapsis
99.1756°
True anomaly
260.94787°
Mean anomaly
260.9785°
Eccentric anomaly
260.96318°
Mean motion
3.80064 °/min
Orbital period
94.72 mins
BSTAR
0.00019457
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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 | 2025-11-24 19:53:33.172Z | 39.232° NE | 2025-11-24 19:56:33.172Z | 100.74° ESE | 24.802° | 2025-11-24 19:59:33.172Z | 156.367° SSE |
| 5 mins | 2025-11-25 08:06:33.172Z | 203.229° SW | 2025-11-25 08:08:33.172Z | 265.791° W | 33.31° | 2025-11-25 08:11:33.172Z | 330.73° NNW |
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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