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 64098U 26145.10604826 +.00000000 +00000-0 +88195-3 0 00009
2 64098 53.1589 31.0063 0001021 92.4647 267.6472 15.34407206 05
| Epoch (UTC): | 25 May 2026 02:32:42 |
| Eccentricity: | 0.0001021 |
| inclination: | 53.1589° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 31.0063° |
| argument of perigee: | 92.4647° |
| revolutions per day: | 15.34407206 |
| mean anomaly at epoch: | 267.6472° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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