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 45573U 26145.43363141 +.00000000 +00000-0 +10362-2 0 00004
2 45573 53.0433 47.4120 0004833 84.5432 275.6132 15.60677683 01
| Epoch (UTC): | 25 May 2026 10:24:25 |
| Eccentricity: | 0.0004833 |
| inclination: | 53.0433° |
| perigee height: | 382 km |
| apogee height: | 389 km |
| right ascension of ascending node: | 47.4120° |
| argument of perigee: | 84.5432° |
| revolutions per day: | 15.60677683 |
| mean anomaly at epoch: | 275.6132° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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