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 53539U 26145.09914741 +.00000000 +00000-0 +44192-4 0 00005
2 53539 53.2132 91.1048 0001355 70.6075 289.5064 15.08842570 09
| Epoch (UTC): | 25 May 2026 02:22:46 |
| Eccentricity: | 0.0001355 |
| inclination: | 53.2132° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 91.1048° |
| argument of perigee: | 70.6075° |
| revolutions per day: | 15.08842570 |
| mean anomaly at epoch: | 289.5064° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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