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 45608U 26145.08969843 +.00000000 +00000-0 +00000-0 0 00001
2 45608 63.1557 69.6031 7075176 266.1794 17.7575 2.00612562 01
| Epoch (UTC): | 25 May 2026 02:09:09 |
| Eccentricity: | 0.7075176 |
| inclination: | 63.1557° |
| perigee height: | 1389 km |
| apogee height: | 38967 km |
| right ascension of ascending node: | 69.6031° |
| argument of perigee: | 266.1794° |
| revolutions per day: | 2.00612562 |
| mean anomaly at epoch: | 17.7575° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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