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 64045U 26145.40238727 +.00000000 +00000-0 +68147-4 0 00003
2 64045 70.0003 281.0038 0002587 275.8204 84.2660 14.98342756 08
| Epoch (UTC): | 25 May 2026 09:39:26 |
| Eccentricity: | 0.0002587 |
| inclination: | 70.0003° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 281.0038° |
| argument of perigee: | 275.8204° |
| revolutions per day: | 14.98342756 |
| mean anomaly at epoch: | 84.2660° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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