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 64804U 26145.44033751 +.00000000 +00000-0 +18991-3 0 00001
2 64804 70.0006 300.9208 0002732 267.5169 92.5677 14.98336318 01
| Epoch (UTC): | 25 May 2026 10:34:05 |
| Eccentricity: | 0.0002732 |
| inclination: | 70.0006° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 300.9208° |
| argument of perigee: | 267.5169° |
| revolutions per day: | 14.98336318 |
| mean anomaly at epoch: | 92.5677° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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