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 64568U 26145.61473117 +.00000000 +00000-0 +16251-3 0 00008
2 64568 97.7707 260.0737 0001729 63.4783 296.6613 14.91842615 07
| Epoch (UTC): | 25 May 2026 14:45:12 |
| Eccentricity: | 0.0001729 |
| inclination: | 97.7707° |
| perigee height: | 591 km |
| apogee height: | 593 km |
| right ascension of ascending node: | 260.0737° |
| argument of perigee: | 63.4783° |
| revolutions per day: | 14.91842615 |
| mean anomaly at epoch: | 296.6613° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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