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 59233U 26145.50284669 +.00000000 +00000-0 +20549-4 0 00007
2 59233 43.0025 69.7396 0000831 292.9344 67.1420 15.27580161 09
| Epoch (UTC): | 25 May 2026 12:04:05 |
| Eccentricity: | 0.0000831 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 69.7396° |
| argument of perigee: | 292.9344° |
| revolutions per day: | 15.27580161 |
| mean anomaly at epoch: | 67.1420° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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