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 12780U 26071.63528718 +.00000000 +00000-0 +62789-3 0 00002
2 12780 82.9487 147.9934 0023034 66.2591 87.9202 13.91464799 07
| Epoch (UTC): | 12 March 2026 15:14:48 |
| Eccentricity: | 0.0023034 |
| inclination: | 82.9487° |
| perigee height: | 907 km |
| apogee height: | 940 km |
| right ascension of ascending node: | 147.9934° |
| argument of perigee: | 66.2591° |
| revolutions per day: | 13.91464799 |
| mean anomaly at epoch: | 87.9202° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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