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 26140.97417777 +.00000000 +00000-0 +67168-4 0 00000
2 11416 98.5648 170.6537 0009422 346.0885 14.0039 14.35479075 07
| Epoch (UTC): | 20 May 2026 23:22:48 |
| Eccentricity: | 0.0009422 |
| inclination: | 98.5648° |
| perigee height: | 767 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 170.6537° |
| argument of perigee: | 346.0885° |
| revolutions per day: | 14.35479075 |
| mean anomaly at epoch: | 14.0039° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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