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 53410U 26145.34938363 +.00000000 +00000-0 +49535-4 0 00003
2 53410 53.2128 129.9812 0000914 88.8578 271.2519 15.08846151 02
| Epoch (UTC): | 25 May 2026 08:23:06 |
| Eccentricity: | 0.0000914 |
| inclination: | 53.2128° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 129.9812° |
| argument of perigee: | 88.8578° |
| revolutions per day: | 15.08846151 |
| mean anomaly at epoch: | 271.2519° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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