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 26041.30179008 +.00000000 +00000-0 +53298-3 0 00001
2 28647 56.9998 4.3168 0058831 328.3400 31.4119 15.41468470 01
| Epoch (UTC): | 10 February 2026 07:14:34 |
| Eccentricity: | 0.0058831 |
| inclination: | 56.9998° |
| perigee height: | 402 km |
| apogee height: | 482 km |
| right ascension of ascending node: | 4.3168° |
| argument of perigee: | 328.3400° |
| revolutions per day: | 15.41468470 |
| mean anomaly at epoch: | 31.4119° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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