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 28538U 26074.96309604 +.00000000 +00000-0 +93950-4 0 00005
2 28538 63.8243 162.9083 0214863 260.4418 97.2274 13.43369669 03
| Epoch (UTC): | 15 March 2026 23:06:51 |
| Eccentricity: | 0.0214863 |
| inclination: | 63.8243° |
| perigee height: | 936 km |
| apogee height: | 1257 km |
| right ascension of ascending node: | 162.9083° |
| argument of perigee: | 260.4418° |
| revolutions per day: | 13.43369669 |
| mean anomaly at epoch: | 97.2274° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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