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 26073.54110321 +.00000000 +00000-0 +11808-3 0 00003
2 28059 98.6882 68.6364 0047446 215.8095 143.9918 14.55025532 02
| Epoch (UTC): | 14 March 2026 12:59:11 |
| Eccentricity: | 0.0047446 |
| inclination: | 98.6882° |
| perigee height: | 676 km |
| apogee height: | 743 km |
| right ascension of ascending node: | 68.6364° |
| argument of perigee: | 215.8095° |
| revolutions per day: | 14.55025532 |
| mean anomaly at epoch: | 143.9918° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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