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 26075.80092134 +.00000000 +00000-0 +11105-3 0 00004
2 11416 98.5740 105.9112 0010159 165.8639 194.2833 14.35438960 04
| Epoch (UTC): | 16 March 2026 19:13:19 |
| Eccentricity: | 0.0010159 |
| inclination: | 98.5740° |
| perigee height: | 766 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 105.9112° |
| argument of perigee: | 165.8639° |
| revolutions per day: | 14.35438960 |
| mean anomaly at epoch: | 194.2833° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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