GHGSAT-C12, 64529
Orbit data source: Space-Track
GHGSAT-C12, 64529 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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64529 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-C12
1 64529U 25135B 26289.92069620 .00005906 00000-0 26908-3 0 9991
2 64529 97.4855 43.7834 0006250 104.6835 255.5094 15.21034630 73325Epoch: 2026-10-16T22:05Z
TLE epoch observation values (Epoch: 2026-10-16T22:05:48.151Z)
Latitude
0°
Longitude
46.89799°
Altitude
506.887 km
Speed
7.61 km/s
True Right ascension
02h 55m 08s
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
04:08:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.985 km
Perigee altitude
495.388 km
Semi-major axis
6,877.823 km
Eccentricity
0.00063
Inclination
97.4855°
RAAN
43.7834°
Arg. of periapsis
104.6835°
True anomaly
255.44007°
Mean anomaly
255.5094°
Eccentric anomaly
255.47473°
Mean motion
3.8051 °/min
Orbital period
94.61 mins
BSTAR
0.00026908
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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-C12 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-10-17 20:45:10.465Z | 5.895° NNE | 2026-10-17 20:48:10.465Z | 329.715° NNW | 57.818° | 2026-10-17 20:52:10.465Z | 202.184° SSW |
| 5 mins | 2026-10-18 07:24:10.465Z | 132.561° SE | 2026-10-18 07:26:10.465Z | 66.011° ENE | 43.133° | 2026-10-18 07:29:10.465Z | 3.493° 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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