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 26072.94300719 +.00000000 +00000-0 +13340-3 0 00000
2 11416 98.5745 103.0708 0009981 174.2644 185.8658 14.35437115 02
| Epoch (UTC): | 13 March 2026 22:37:55 |
| Eccentricity: | 0.0009981 |
| inclination: | 98.5745° |
| perigee height: | 766 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 103.0708° |
| argument of perigee: | 174.2644° |
| revolutions per day: | 14.35437115 |
| mean anomaly at epoch: | 185.8658° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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