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: 8 hours ago
TLE from 8 hours ago
0 GHGSAT-C13
1 64548U 25135W 26062.50404664 .00004764 00000-0 22321-3 0 9992
2 64548 97.4646 178.8032 0002567 107.1539 252.9978 15.20182434 38799Epoch: 2026-03-03T12:05Z
TLE epoch observation values (Epoch: 2026-03-03T12:05:49.629Z)
Latitude
0.00004°
Longitude
-163.93575°
Altitude
508.896 km
Speed
7.609 km/s
True Right ascension
11h 55m 12s
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
23:38:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.024 km
Perigee altitude
500.492 km
Semi-major axis
6,880.395 km
Eccentricity
0.00026
Inclination
97.4646°
RAAN
178.8032°
Arg. of periapsis
107.1539°
True anomaly
252.96967°
Mean anomaly
252.9978°
Eccentric anomaly
252.98374°
Mean motion
3.80297 °/min
Orbital period
94.66 mins
BSTAR
0.00022321
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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 | 2026-03-03 20:33:13.670Z | 11.444° NNE | 2026-03-03 20:36:13.670Z | 3.668° NNE | 44.248° | 2026-03-03 20:39:13.670Z | 193.922° SSW |
| 5 mins | 2026-03-04 07:12:13.670Z | 125.396° SE | 2026-03-04 07:14:13.670Z | 73.243° E | 29.077° | 2026-03-04 07:17:13.670Z | 9.604° 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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