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 52603U 26145.15669775 +.00000000 +00000-0 +56665-3 0 00004
2 52603 53.2165 295.8554 0001541 88.5491 271.5678 15.08805281 08
| Epoch (UTC): | 25 May 2026 03:45:38 |
| Eccentricity: | 0.0001541 |
| inclination: | 53.2165° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 295.8554° |
| argument of perigee: | 88.5491° |
| revolutions per day: | 15.08805281 |
| mean anomaly at epoch: | 271.5678° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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