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 59588U 26137.39856968 +.00000000 +00000-0 +39504-3 0 00005
2 59588 97.1717 63.0800 0024488 354.8515 5.2395 13.92753301 01
| Epoch (UTC): | 17 May 2026 09:33:56 |
| Eccentricity: | 0.0024488 |
| inclination: | 97.1717° |
| perigee height: | 901 km |
| apogee height: | 937 km |
| right ascension of ascending node: | 63.0800° |
| argument of perigee: | 354.8515° |
| revolutions per day: | 13.92753301 |
| mean anomaly at epoch: | 5.2395° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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