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 26018.59486440 +.00000000 +00000-0 +11200-3 0 00001
2 28059 98.6819 11.5581 0048747 25.8433 334.5182 14.54951935 05
| Epoch (UTC): | 18 January 2026 14:16:36 |
| Eccentricity: | 0.0048747 |
| inclination: | 98.6819° |
| perigee height: | 675 km |
| apogee height: | 744 km |
| right ascension of ascending node: | 11.5581° |
| argument of perigee: | 25.8433° |
| revolutions per day: | 14.54951935 |
| mean anomaly at epoch: | 334.5182° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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