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 26039.50081220 +.00000000 +00000-0 +15446-3 0 00008
2 28059 98.6848 33.2682 0047476 321.9585 37.8261 14.54987841 02
| Epoch (UTC): | 08 February 2026 12:01:10 |
| Eccentricity: | 0.0047476 |
| inclination: | 98.6848° |
| perigee height: | 676 km |
| apogee height: | 743 km |
| right ascension of ascending node: | 33.2682° |
| argument of perigee: | 321.9585° |
| revolutions per day: | 14.54987841 |
| mean anomaly at epoch: | 37.8261° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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