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 45430U 26145.64419763 +.00000000 +00000-0 +85392-2 0 00006
2 45430 87.8879 25.5596 0001389 66.9341 293.1933 13.10885222 09
| Epoch (UTC): | 25 May 2026 15:27:38 |
| Eccentricity: | 0.0001389 |
| inclination: | 87.8879° |
| perigee height: | 1219 km |
| apogee height: | 1221 km |
| right ascension of ascending node: | 25.5596° |
| argument of perigee: | 66.9341° |
| revolutions per day: | 13.10885222 |
| mean anomaly at epoch: | 293.1933° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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