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: 11 hours ago
TLE from 11 hours ago
0 GHGSAT-C13
1 64548U 25135W 26289.90441196 .00005598 00000-0 24623-3 0 9991
2 64548 97.4887 44.5816 0002263 74.3896 285.7590 15.22280233 73363Epoch: 2026-10-16T21:42Z
TLE epoch observation values (Epoch: 2026-10-16T21:42:21.193Z)
Latitude
0.00001°
Longitude
53.57456°
Altitude
501.633 km
Speed
7.614 km/s
True Right ascension
02h 58m 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
03:11:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
497.486 km
Perigee altitude
494.375 km
Semi-major axis
6,874.068 km
Eccentricity
0.00023
Inclination
97.4887°
RAAN
44.5816°
Arg. of periapsis
74.3896°
True anomaly
285.73404°
Mean anomaly
285.759°
Eccentric anomaly
285.74652°
Mean motion
3.80822 °/min
Orbital period
94.53 mins
BSTAR
0.00024623
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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 | 2026-10-17 20:22:43.133Z | 37.183° NE | 2026-10-17 20:24:43.133Z | 119.525° SE | 48.514° | 2026-10-17 20:27:43.133Z | 175.528° S |
| 5 mins | 2026-10-18 06:58:43.133Z | 116.693° SE | 2026-10-18 07:01:43.133Z | 61.411° ENE | 19.743° | 2026-10-18 07:03:43.133Z | 25.505° NE |
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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