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 26073.90681626 +.00000000 +00000-0 +51200-3 0 00007
2 28647 56.9958 224.2012 0062422 29.4100 331.0444 15.42901929 07
| Epoch (UTC): | 14 March 2026 21:45:48 |
| Eccentricity: | 0.0062422 |
| inclination: | 56.9958° |
| perigee height: | 395 km |
| apogee height: | 480 km |
| right ascension of ascending node: | 224.2012° |
| argument of perigee: | 29.4100° |
| revolutions per day: | 15.42901929 |
| mean anomaly at epoch: | 331.0444° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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