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 59387U 26144.67605806 +.00000000 +00000-0 +28798-3 0 00007
2 59387 53.1583 262.8288 0002425 79.6843 280.4433 15.33557415 08
| Epoch (UTC): | 24 May 2026 16:13:31 |
| Eccentricity: | 0.0002425 |
| inclination: | 53.1583° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 262.8288° |
| argument of perigee: | 79.6843° |
| revolutions per day: | 15.33557415 |
| mean anomaly at epoch: | 280.4433° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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