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 00045U 26106.86777639 +.00000000 +00000-0 +57434-4 0 00007
2 00045 66.6925 162.3894 0251857 205.4872 153.3638 14.35934649 01
| Epoch (UTC): | 16 April 2026 20:49:35 |
| Eccentricity: | 0.0251857 |
| inclination: | 66.6925° |
| perigee height: | 592 km |
| apogee height: | 952 km |
| right ascension of ascending node: | 162.3894° |
| argument of perigee: | 205.4872° |
| revolutions per day: | 14.35934649 |
| mean anomaly at epoch: | 153.3638° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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