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 26133.05861345 +.00000000 +00000-0 +41162-4 0 00006
2 00116 66.8102 336.7904 0081540 295.5231 63.7432 13.92325791 07
| Epoch (UTC): | 13 May 2026 01:24:24 |
| Eccentricity: | 0.0081540 |
| inclination: | 66.8102° |
| perigee height: | 861 km |
| apogee height: | 980 km |
| right ascension of ascending node: | 336.7904° |
| argument of perigee: | 295.5231° |
| revolutions per day: | 13.92325791 |
| mean anomaly at epoch: | 63.7432° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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