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 59008U 26145.51519566 +.00000000 +00000-0 +22688-4 0 00001
2 59008 53.1603 81.4208 0001164 89.7409 270.3725 15.30196120 08
| Epoch (UTC): | 25 May 2026 12:21:52 |
| Eccentricity: | 0.0001164 |
| inclination: | 53.1603° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 81.4208° |
| argument of perigee: | 89.7409° |
| revolutions per day: | 15.30196120 |
| mean anomaly at epoch: | 270.3725° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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