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 26072.92219410 +.00000000 +00000-0 +11300-3 0 00000
2 28059 98.6880 67.9930 0047422 217.7404 142.0463 14.55024700 01
| Epoch (UTC): | 13 March 2026 22:07:57 |
| Eccentricity: | 0.0047422 |
| inclination: | 98.6880° |
| perigee height: | 676 km |
| apogee height: | 743 km |
| right ascension of ascending node: | 67.9930° |
| argument of perigee: | 217.7404° |
| revolutions per day: | 14.55024700 |
| mean anomaly at epoch: | 142.0463° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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