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 64758U 26145.42540646 +.00000000 +00000-0 +41541-3 0 00000
2 64758 53.1581 245.3790 0001090 25.1030 335.0026 15.34388651 09
| Epoch (UTC): | 25 May 2026 10:12:35 |
| Eccentricity: | 0.0001090 |
| inclination: | 53.1581° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 245.3790° |
| argument of perigee: | 25.1030° |
| revolutions per day: | 15.34388651 |
| mean anomaly at epoch: | 335.0026° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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