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 00116U 26140.96016095 +.00000000 +00000-0 +40628-4 0 00004
2 00116 66.8096 317.4544 0081781 290.3860 68.8449 13.92326625 04
| Epoch (UTC): | 20 May 2026 23:02:37 |
| Eccentricity: | 0.0081781 |
| inclination: | 66.8096° |
| perigee height: | 861 km |
| apogee height: | 980 km |
| right ascension of ascending node: | 317.4544° |
| argument of perigee: | 290.3860° |
| revolutions per day: | 13.92326625 |
| mean anomaly at epoch: | 68.8449° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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