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 45431U 26145.60353865 +.00000000 +00000-0 -80663-3 0 00001
2 45431 87.8904 25.5691 0001608 80.5633 279.5677 13.11413886 02
| Epoch (UTC): | 25 May 2026 14:29:05 |
| Eccentricity: | 0.0001608 |
| inclination: | 87.8904° |
| perigee height: | 1216 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.5691° |
| argument of perigee: | 80.5633° |
| revolutions per day: | 13.11413886 |
| mean anomaly at epoch: | 279.5677° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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