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 64579U 26145.57261632 +.00000000 +00000-0 +97766-4 0 00003
2 64579 97.7740 260.1021 0004335 77.6501 282.5204 14.93049141 09
| Epoch (UTC): | 25 May 2026 13:44:34 |
| Eccentricity: | 0.0004335 |
| inclination: | 97.7740° |
| perigee height: | 585 km |
| apogee height: | 591 km |
| right ascension of ascending node: | 260.1021° |
| argument of perigee: | 77.6501° |
| revolutions per day: | 14.93049141 |
| mean anomaly at epoch: | 282.5204° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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