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 28117U 26139.73239337 +.00000000 +00000-0 +00000-0 0 00000
2 28117 8.9376 33.9705 0002526 19.0332 163.5186 1.00272827 03
| Epoch (UTC): | 19 May 2026 17:34:38 |
| Eccentricity: | 0.0002526 |
| inclination: | 8.9376° |
| perigee height: | 35776 km |
| apogee height: | 35797 km |
| right ascension of ascending node: | 33.9705° |
| argument of perigee: | 19.0332° |
| revolutions per day: | 1.00272827 |
| mean anomaly at epoch: | 163.5186° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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