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, Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 GHGSAT-C12
1 64529U 25135B 26104.92116542 .00002141 00000-0 10298-3 0 9996
2 64529 97.4663 220.3362 0005880 48.0678 312.1057 15.19875678 45213Epoch: 2026-04-14T22:06Z
TLE epoch observation values (Epoch: 2026-04-14T22:06:28.692Z)
Latitude
-0.00004°
Longitude
45.62617°
Altitude
506.591 km
Speed
7.612 km/s
True Right ascension
14h 41m 20s
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
14:09:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
507.231 km
Perigee altitude
499.138 km
Semi-major axis
6,881.322 km
Eccentricity
0.00059
Inclination
97.4663°
RAAN
220.3362°
Arg. of periapsis
48.0678°
True anomaly
312.05569°
Mean anomaly
312.1057°
Eccentric anomaly
312.0807°
Mean motion
3.8022 °/min
Orbital period
94.68 mins
BSTAR
0.00010298
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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 | 2026-04-15 07:42:30.180Z | 168.439° S | 2026-04-15 07:45:30.180Z | 179.249° S | 43.41° | 2026-04-15 07:49:30.180Z | 347.147° N |
| 5 mins | 2026-04-15 20:48:30.180Z | 351.443° N | 2026-04-15 20:50:30.180Z | 268.747° W | 38.744° | 2026-04-15 20:53:30.180Z | 208.766° SW |
| 5 mins | 2026-04-16 07:26:30.180Z | 138.985° SSE | 2026-04-16 07:28:30.180Z | 50.997° ENE | 37.776° | 2026-04-16 07:31:30.180Z | 358.53° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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