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 59418U 26145.57526929 +.00000000 +00000-0 +52353-4 0 00005
2 59418 43.0039 342.0310 0001248 271.6462 88.4247 15.27566572 03
| Epoch (UTC): | 25 May 2026 13:48:23 |
| Eccentricity: | 0.0001248 |
| inclination: | 43.0039° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 342.0310° |
| argument of perigee: | 271.6462° |
| revolutions per day: | 15.27566572 |
| mean anomaly at epoch: | 88.4247° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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