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 53562U 26145.20036181 +.00000000 +00000-0 +11231-4 0 00005
2 53562 53.2136 70.7932 0001191 74.2911 285.8213 15.08843855 03
| Epoch (UTC): | 25 May 2026 04:48:31 |
| Eccentricity: | 0.0001191 |
| inclination: | 53.2136° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 70.7932° |
| argument of perigee: | 74.2911° |
| revolutions per day: | 15.08843855 |
| mean anomaly at epoch: | 285.8213° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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