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 28659U 26145.56015499 +.00000000 +00000-0 +00000-0 0 00000
2 28659 0.0158 343.4900 0003258 88.7682 253.4894 1.00272345 05
| Epoch (UTC): | 25 May 2026 13:26:37 |
| Eccentricity: | 0.0003258 |
| inclination: | 0.0158° |
| perigee height: | 35773 km |
| apogee height: | 35800 km |
| right ascension of ascending node: | 343.4900° |
| argument of perigee: | 88.7682° |
| revolutions per day: | 1.00272345 |
| mean anomaly at epoch: | 253.4894° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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