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 26162.44483148 +.00000000 +00000-0 +27766-3 0 00004
2 28647 56.9952 202.3347 0052961 189.6729 170.3313 15.46297549 01
| Epoch (UTC): | 11 June 2026 10:40:33 |
| Eccentricity: | 0.0052961 |
| inclination: | 56.9952° |
| perigee height: | 392 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 202.3347° |
| argument of perigee: | 189.6729° |
| revolutions per day: | 15.46297549 |
| mean anomaly at epoch: | 170.3313° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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