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 26134.99808457 +.00000000 +00000-0 +42016-4 0 00004
2 00116 66.8100 332.0443 0081602 294.2660 64.9911 13.92325962 08
| Epoch (UTC): | 14 May 2026 23:57:14 |
| Eccentricity: | 0.0081602 |
| inclination: | 66.8100° |
| perigee height: | 861 km |
| apogee height: | 980 km |
| right ascension of ascending node: | 332.0443° |
| argument of perigee: | 294.2660° |
| revolutions per day: | 13.92325962 |
| mean anomaly at epoch: | 64.9911° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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