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 45437U 26145.42423872 +.00000000 +00000-0 +13464-2 0 00006
2 45437 87.8915 25.5910 0001990 89.2045 270.9311 13.11953970 04
| Epoch (UTC): | 25 May 2026 10:10:54 |
| Eccentricity: | 0.0001990 |
| inclination: | 87.8915° |
| perigee height: | 1214 km |
| apogee height: | 1217 km |
| right ascension of ascending node: | 25.5910° |
| argument of perigee: | 89.2045° |
| revolutions per day: | 13.11953970 |
| mean anomaly at epoch: | 270.9311° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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