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GHGSAT-C12

In orbit NORAD 64529 NBMM-3117-5947-3620-0744

Observations 0
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Falcon 9 Block 5 | Transporter 14 (Dedicated SSO Rideshare)

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
GHGSAT-C12
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Launch
Falcon 9 Block 5 | Transporter 14 (Dedicated SSO Rideshare)
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
495.70 km
Apogee
504.10 km
Inclination
97.5°
Period
94.7 min
Semi-major axis
6878.0 km
Velocity
7.6 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 12:56:45 UTC
Two-line elements (TLE)
1 64529U 25135B   26284.19712541  .00007138  00000-0  32518-3 0  9995
2 64529  97.4858  38.0962 0006108 120.3849 239.7990 15.20964825 72458
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Orbit history, past year

Mean elements of every TLE set over the past 365 days, plotted against the epoch of the set. Each source is its own line; click it in the legend to hide it. A jump in altitude is a manoeuvre or a bad set; lines drifting apart are a disagreement between sources. “TLE age” is how many hours have passed since the epoch of the source's freshest set, plotted against when the set reached us, on a logarithmic scale. A set the source repeats unchanged does not reset the age.

Prediction divergence

Each TLE set is propagated with SGP4 to the epoch of the next set from the same source and compared with it, plotted against the epoch of the next set; the tooltip shows how many hours ahead the prediction ran. The logarithmic scale shows the size of the divergence and the tooltip its sign: plus along-track means the prediction is ahead of the satellite. This is how well the sets agree, not the true error: the reference is a TLE too, off by about a kilometre. An outlier is a manoeuvre between sets. Sets more than a week apart are not compared.

Time of closest approach, UTC Object 1 Object 2 Distance, km Speed, km/s Max. probability
2026-10-12 06:44:59 GHGSAT-C12
NORAD 64529 		TOMORROW-S8
NORAD 66308 		4.319 14.43 1.1e-07
2026-10-12 07:58:45 GHGSAT-C12
NORAD 64529 		FLOCK 4H-15
NORAD 66718 		1.555 5.45 1.7e-06
2026-10-12 08:03:38 GHGSAT-C12
NORAD 64529 		FENGYUN 1C DEB
NORAD 30095 		4.662 14.15 9.9e-08
2026-10-13 03:23:21 STARLINK-5016
NORAD 56143 		GHGSAT-C12
NORAD 64529 		2.366 7.41 2.1e-05
2026-10-13 18:42:55 GHGSAT-C12
NORAD 64529 		FLOCK 4H-7
NORAD 66710 		2.417 5.45 7.1e-07
2026-10-14 09:42:53 GHGSAT-C12
NORAD 64529 		AC1-002
NORAD 66745 		4.719 5.50 1.9e-07
2026-10-15 11:45:59 GHGSAT-C12
NORAD 64529 		BLACK KITE-1
NORAD 66741 		4.654 5.40 1.9e-07
2026-10-15 14:06:43 GHGSAT-C12
NORAD 64529 		RASSVET-3 5
NORAD 68364 		4.982 14.68 7.3e-08
2026-10-15 22:15:22 GHGSAT-C12
NORAD 64529 		ELECTRON KICK STAGE R/B
NORAD 100563 		3.241 12.77 2.6e-07
2026-10-16 10:51:45 GHGSAT-C12
NORAD 64529 		CZ-2C DEB
NORAD 37735 		4.537 14.94 8.1e-08
2026-10-16 23:19:51 GHGSAT-C12
NORAD 64529 		HYDRA-2
NORAD 67389 		3.809 12.79 1.9e-07
2026-10-17 01:00:02 GHGSAT-C12
NORAD 64529 		HADES-SA (SPINNYONE)
NORAD 68446 		4.750 14.76 7.8e-08

Data: CelesTrak SOCRATES Plus, computed from TLEs of the public catalog. This is an estimate, not grounds for a manoeuvre: TLEs carry no covariance, and the maximum probability assumes a position error.

All conjunctions of this satellite