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 26064.09041564 +.00000000 +00000-0 +15861-3 0 00007
2 11416 98.5756 94.2718 0009482 200.8263 159.2537 14.35429614 01
| Epoch (UTC): | 05 March 2026 02:10:11 |
| Eccentricity: | 0.0009482 |
| inclination: | 98.5756° |
| perigee height: | 767 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 94.2718° |
| argument of perigee: | 200.8263° |
| revolutions per day: | 14.35429614 |
| mean anomaly at epoch: | 159.2537° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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