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 64587U 26145.60393865 +.00000000 +00000-0 +17652-3 0 00005
2 64587 97.7710 260.4072 0002973 79.8839 280.2715 14.91852617 08
| Epoch (UTC): | 25 May 2026 14:29:40 |
| Eccentricity: | 0.0002973 |
| inclination: | 97.7710° |
| perigee height: | 590 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 260.4072° |
| argument of perigee: | 79.8839° |
| revolutions per day: | 14.91852617 |
| mean anomaly at epoch: | 280.2715° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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