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 26144.74312219 +.00000000 +00000-0 +00000-0 0 00008
2 28117 8.9369 33.9479 0002465 38.1108 153.2802 1.00273183 05
| Epoch (UTC): | 24 May 2026 17:50:05 |
| Eccentricity: | 0.0002465 |
| inclination: | 8.9369° |
| perigee height: | 35776 km |
| apogee height: | 35797 km |
| right ascension of ascending node: | 33.9479° |
| argument of perigee: | 38.1108° |
| revolutions per day: | 1.00273183 |
| mean anomaly at epoch: | 153.2802° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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