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 00016U 26133.14395147 +.00000000 +00000-0 -11843-4 0 00001
2 00016 34.2698 46.3903 2018418 332.5235 18.1434 10.49588387 07
| Epoch (UTC): | 13 May 2026 03:27:17 |
| Eccentricity: | 0.2018418 |
| inclination: | 34.2698° |
| perigee height: | 655 km |
| apogee height: | 4212 km |
| right ascension of ascending node: | 46.3903° |
| argument of perigee: | 332.5235° |
| revolutions per day: | 10.49588387 |
| mean anomaly at epoch: | 18.1434° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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