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 45237U 26145.52872567 +.00000000 +00000-0 +10659-2 0 00007
2 45237 53.0422 336.8886 0002436 142.6618 217.4564 15.59549769 03
| Epoch (UTC): | 25 May 2026 12:41:21 |
| Eccentricity: | 0.0002436 |
| inclination: | 53.0422° |
| perigee height: | 387 km |
| apogee height: | 391 km |
| right ascension of ascending node: | 336.8886° |
| argument of perigee: | 142.6618° |
| revolutions per day: | 15.59549769 |
| mean anomaly at epoch: | 217.4564° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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