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 64562U 26145.27957995 +.00000000 +00000-0 +21345-3 0 00005
2 64562 97.7726 259.7005 0001238 95.4968 264.6393 14.93698016 06
| Epoch (UTC): | 25 May 2026 06:42:35 |
| Eccentricity: | 0.0001238 |
| inclination: | 97.7726° |
| perigee height: | 586 km |
| apogee height: | 587 km |
| right ascension of ascending node: | 259.7005° |
| argument of perigee: | 95.4968° |
| revolutions per day: | 14.93698016 |
| mean anomaly at epoch: | 264.6393° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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