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 59089U 26145.51912942 +.00000000 +00000-0 +43416-4 0 00007
2 59089 43.0026 236.6410 0001483 263.5319 96.5364 15.27579290 05
| Epoch (UTC): | 25 May 2026 12:27:32 |
| Eccentricity: | 0.0001483 |
| inclination: | 43.0026° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 236.6410° |
| argument of perigee: | 263.5319° |
| revolutions per day: | 15.27579290 |
| mean anomaly at epoch: | 96.5364° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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