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 28647U 26065.54777473 +.00000000 +00000-0 +49717-3 0 00004
2 28647 56.9965 260.1529 0061305 14.3646 345.9133 15.42523200 05
| Epoch (UTC): | 06 March 2026 13:08:47 |
| Eccentricity: | 0.0061305 |
| inclination: | 56.9965° |
| perigee height: | 397 km |
| apogee height: | 480 km |
| right ascension of ascending node: | 260.1529° |
| argument of perigee: | 14.3646° |
| revolutions per day: | 15.42523200 |
| mean anomaly at epoch: | 345.9133° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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