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 59239U 26145.47216564 +.00000000 +00000-0 +22239-4 0 00006
2 59239 43.0018 59.0597 0000997 272.4484 87.6253 15.27584648 08
| Epoch (UTC): | 25 May 2026 11:19:55 |
| Eccentricity: | 0.0000997 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 59.0597° |
| argument of perigee: | 272.4484° |
| revolutions per day: | 15.27584648 |
| mean anomaly at epoch: | 87.6253° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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