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 53908U 26145.53340824 +.00000000 +00000-0 -11727-4 0 00008
2 53908 53.2129 329.2967 0001591 89.0160 271.1014 15.08834649 01
| Epoch (UTC): | 25 May 2026 12:48:06 |
| Eccentricity: | 0.0001591 |
| inclination: | 53.2129° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 329.2967° |
| argument of perigee: | 89.0160° |
| revolutions per day: | 15.08834649 |
| mean anomaly at epoch: | 271.1014° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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