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 13778U 26042.11902014 +.00000000 +00000-0 +59200-4 0 00001
2 13778 100.0818 79.8621 0020211 262.1006 97.7866 14.09686522 08
| Epoch (UTC): | 11 February 2026 02:51:23 |
| Eccentricity: | 0.0020211 |
| inclination: | 100.0818° |
| perigee height: | 846 km |
| apogee height: | 875 km |
| right ascension of ascending node: | 79.8621° |
| argument of perigee: | 262.1006° |
| revolutions per day: | 14.09686522 |
| mean anomaly at epoch: | 97.7866° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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