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 45446U 26145.11172367 +.00000000 +00000-0 +13703-2 0 00008
2 45446 87.8919 25.6529 0001929 76.9941 283.1402 13.11417238 04
| Epoch (UTC): | 25 May 2026 02:40:52 |
| Eccentricity: | 0.0001929 |
| inclination: | 87.8919° |
| perigee height: | 1216 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.6529° |
| argument of perigee: | 76.9941° |
| revolutions per day: | 13.11417238 |
| mean anomaly at epoch: | 283.1402° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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