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 59068U 26145.63740580 +.00000000 +00000-0 +26829-3 0 00002
2 59068 95.3922 219.7617 0146044 46.8373 314.4951 14.93559667 05
| Epoch (UTC): | 25 May 2026 15:17:51 |
| Eccentricity: | 0.0146044 |
| inclination: | 95.3922° |
| perigee height: | 485 km |
| apogee height: | 689 km |
| right ascension of ascending node: | 219.7617° |
| argument of perigee: | 46.8373° |
| revolutions per day: | 14.93559667 |
| mean anomaly at epoch: | 314.4951° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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