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 56458U 26145.45906919 +.00000000 +00000-0 +44034-4 0 00001
2 56458 69.9987 310.9597 0002733 269.7612 90.3233 14.98330529 04
| Epoch (UTC): | 25 May 2026 11:01:03 |
| Eccentricity: | 0.0002733 |
| inclination: | 69.9987° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 310.9597° |
| argument of perigee: | 269.7612° |
| revolutions per day: | 14.98330529 |
| mean anomaly at epoch: | 90.3233° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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