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 59447U 26145.65585449 +.00000000 +00000-0 +41374-3 0 00008
2 59447 45.6052 3.5566 0001967 217.1605 142.9144 15.08581766 05
| Epoch (UTC): | 25 May 2026 15:44:25 |
| Eccentricity: | 0.0001967 |
| inclination: | 45.6052° |
| perigee height: | 539 km |
| apogee height: | 542 km |
| right ascension of ascending node: | 3.5566° |
| argument of perigee: | 217.1605° |
| revolutions per day: | 15.08581766 |
| mean anomaly at epoch: | 142.9144° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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