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: 7 hours ago
TLE from 7 hours ago
0 GHGSAT-C12
1 64529U 25135B 26225.17561569 .00001573 00000-0 74964-4 0 9999
2 64529 97.4791 339.5041 0004348 354.0620 6.0563 15.20595695 63487Epoch: 2026-08-13T04:12Z
TLE epoch observation values (Epoch: 2026-08-13T04:12:53.195Z)
Latitude
-0.00003°
Longitude
-45.33651°
Altitude
504.155 km
Speed
7.614 km/s
True Right ascension
22h 38m 00s
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
01:17:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.002 km
Perigee altitude
498.02 km
Semi-major axis
6,879.148 km
Eccentricity
0.00043
Inclination
97.4791°
RAAN
339.5041°
Arg. of periapsis
354.062°
True anomaly
6.06156°
Mean anomaly
6.0563°
Eccentric anomaly
6.05893°
Mean motion
3.80401 °/min
Orbital period
94.64 mins
BSTAR
0.000074964
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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 | 2026-08-13 20:33:34.497Z | 11.939° NNE | 2026-08-13 20:37:34.497Z | 192.825° SSW | 43.532° | 2026-08-13 20:40:34.497Z | 193.103° SSW |
| 5 mins | 2026-08-14 07:12:34.497Z | 127.188° SE | 2026-08-14 07:14:34.497Z | 80.622° E | 28.263° | 2026-08-14 07:17:34.497Z | 11.786° 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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