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 59498U 26145.35008050 +.00000000 +00000-0 +63891-4 0 00008
2 59498 43.0017 266.4779 0001201 273.0382 87.0332 15.27581549 02
| Epoch (UTC): | 25 May 2026 08:24:06 |
| Eccentricity: | 0.0001201 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 266.4779° |
| argument of perigee: | 273.0382° |
| revolutions per day: | 15.27581549 |
| mean anomaly at epoch: | 87.0332° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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