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 45366U 26145.47102735 +.00000000 +00000-0 +10022-2 0 00001
2 45366 53.1540 168.3240 0003911 26.9342 333.1862 15.32690663 05
| Epoch (UTC): | 25 May 2026 11:18:16 |
| Eccentricity: | 0.0003911 |
| inclination: | 53.1540° |
| perigee height: | 465 km |
| apogee height: | 470 km |
| right ascension of ascending node: | 168.3240° |
| argument of perigee: | 26.9342° |
| revolutions per day: | 15.32690663 |
| mean anomaly at epoch: | 333.1862° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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