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 28059U 26105.86161154 +.00000000 +00000-0 +57091-4 0 00009
2 28059 98.6899 102.2331 0049185 117.6358 242.9843 14.55053003 03
| Epoch (UTC): | 15 April 2026 20:40:43 |
| Eccentricity: | 0.0049185 |
| inclination: | 98.6899° |
| perigee height: | 674 km |
| apogee height: | 744 km |
| right ascension of ascending node: | 102.2331° |
| argument of perigee: | 117.6358° |
| revolutions per day: | 14.55053003 |
| mean anomaly at epoch: | 242.9843° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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