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 64744U 26145.48910815 +.00000000 +00000-0 +50799-3 0 00005
2 64744 53.1585 184.0687 0000935 86.1861 273.9247 15.30207836 04
| Epoch (UTC): | 25 May 2026 11:44:18 |
| Eccentricity: | 0.0000935 |
| inclination: | 53.1585° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 184.0687° |
| argument of perigee: | 86.1861° |
| revolutions per day: | 15.30207836 |
| mean anomaly at epoch: | 273.9247° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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