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 26071.83343891 +.00000000 +00000-0 +44302-3 0 00001
2 28647 56.9966 233.1210 0062227 25.7084 334.7041 15.42810380 01
| Epoch (UTC): | 12 March 2026 20:00:09 |
| Eccentricity: | 0.0062227 |
| inclination: | 56.9966° |
| perigee height: | 395 km |
| apogee height: | 480 km |
| right ascension of ascending node: | 233.1210° |
| argument of perigee: | 25.7084° |
| revolutions per day: | 15.42810380 |
| mean anomaly at epoch: | 334.7041° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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