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 59270U 26145.42278918 +.00000000 +00000-0 +10086-3 0 00003
2 59270 53.1598 184.7937 0001091 84.5945 275.5180 15.30208440 06
| Epoch (UTC): | 25 May 2026 10:08:48 |
| Eccentricity: | 0.0001091 |
| inclination: | 53.1598° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 184.7937° |
| argument of perigee: | 84.5945° |
| revolutions per day: | 15.30208440 |
| mean anomaly at epoch: | 275.5180° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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