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 26141.20648411 +.00000000 +00000-0 +16538-2 0 00003
2 59588 97.1703 66.0319 0023535 14.9009 345.2845 13.92598614 09
| Epoch (UTC): | 21 May 2026 04:57:20 |
| Eccentricity: | 0.0023535 |
| inclination: | 97.1703° |
| perigee height: | 902 km |
| apogee height: | 937 km |
| right ascension of ascending node: | 66.0319° |
| argument of perigee: | 14.9009° |
| revolutions per day: | 13.92598614 |
| mean anomaly at epoch: | 345.2845° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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