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 64560U 26145.25737589 +.00000000 +00000-0 +42974-3 0 00007
2 64560 97.7702 260.1302 0001228 82.0996 278.0364 14.95389512 03
| Epoch (UTC): | 25 May 2026 06:10:37 |
| Eccentricity: | 0.0001228 |
| inclination: | 97.7702° |
| perigee height: | 580 km |
| apogee height: | 582 km |
| right ascension of ascending node: | 260.1302° |
| argument of perigee: | 82.0996° |
| revolutions per day: | 14.95389512 |
| mean anomaly at epoch: | 278.0364° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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