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 64069U 26145.64090677 +.00000000 +00000-0 +12138-2 0 00002
2 64069 43.0027 355.0061 0002775 254.6595 105.3966 15.70845733 03
| Epoch (UTC): | 25 May 2026 15:22:54 |
| Eccentricity: | 0.0002775 |
| inclination: | 43.0027° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 355.0061° |
| argument of perigee: | 254.6595° |
| revolutions per day: | 15.70845733 |
| mean anomaly at epoch: | 105.3966° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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