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 11416U 26037.95063494 +.00000000 +00000-0 +16805-3 0 00007
2 11416 98.5789 68.2854 0008735 285.9695 74.0528 14.35409752 07
| Epoch (UTC): | 06 February 2026 22:48:54 |
| Eccentricity: | 0.0008735 |
| inclination: | 98.5789° |
| perigee height: | 767 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 68.2854° |
| argument of perigee: | 285.9695° |
| revolutions per day: | 14.35409752 |
| mean anomaly at epoch: | 74.0528° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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