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 26158.88905296 +.00000000 +00000-0 +35610-3 0 00007
2 28647 56.9953 217.7095 0053735 182.7741 177.3025 15.46185616 08
| Epoch (UTC): | 07 June 2026 21:20:14 |
| Eccentricity: | 0.0053735 |
| inclination: | 56.9953° |
| perigee height: | 391 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 217.7095° |
| argument of perigee: | 182.7741° |
| revolutions per day: | 15.46185616 |
| mean anomaly at epoch: | 177.3025° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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