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 56564U 26145.61152615 +.00000000 +00000-0 +00000-0 0 00004
2 56564 0.5139 326.1217 0003863 169.2632 108.0295 1.00272153 03
| Epoch (UTC): | 25 May 2026 14:40:35 |
| Eccentricity: | 0.0003863 |
| inclination: | 0.5139° |
| perigee height: | 35770 km |
| apogee height: | 35803 km |
| right ascension of ascending node: | 326.1217° |
| argument of perigee: | 169.2632° |
| revolutions per day: | 1.00272153 |
| mean anomaly at epoch: | 108.0295° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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