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 64586U 26145.57263477 +.00000000 +00000-0 +35611-3 0 00000
2 64586 97.7653 260.7563 0005128 53.8595 306.3100 14.96470606 04
| Epoch (UTC): | 25 May 2026 13:44:35 |
| Eccentricity: | 0.0005128 |
| inclination: | 97.7653° |
| perigee height: | 574 km |
| apogee height: | 581 km |
| right ascension of ascending node: | 260.7563° |
| argument of perigee: | 53.8595° |
| revolutions per day: | 14.96470606 |
| mean anomaly at epoch: | 306.3100° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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