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 59445U 26145.38729556 +.00000000 +00000-0 +11268-3 0 00004
2 59445 45.6220 36.3712 0003904 292.6152 67.4317 14.99024190 00
| Epoch (UTC): | 25 May 2026 09:17:42 |
| Eccentricity: | 0.0003904 |
| inclination: | 45.6220° |
| perigee height: | 567 km |
| apogee height: | 573 km |
| right ascension of ascending node: | 36.3712° |
| argument of perigee: | 292.6152° |
| revolutions per day: | 14.99024190 |
| mean anomaly at epoch: | 67.4317° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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