View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 12792U 26065.06455760 +.00000000 +00000-0 +99013-4 0 00002
2 12792 74.0282 290.3864 0013347 167.1814 192.9683 14.39007155 07
| Epoch (UTC): | 06 March 2026 01:32:57 |
| Eccentricity: | 0.0013347 |
| inclination: | 74.0282° |
| perigee height: | 752 km |
| apogee height: | 771 km |
| right ascension of ascending node: | 290.3864° |
| argument of perigee: | 167.1814° |
| revolutions per day: | 14.39007155 |
| mean anomaly at epoch: | 192.9683° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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