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 59108U 26088.19862975 +.00000000 +00000-0 +17496-3 0 00007
2 59108 97.8350 219.1795 0006905 258.5535 101.4911 14.96612362 01
| Epoch (UTC): | 29 March 2026 04:46:01 |
| Eccentricity: | 0.0006905 |
| inclination: | 97.8350° |
| perigee height: | 573 km |
| apogee height: | 582 km |
| right ascension of ascending node: | 219.1795° |
| argument of perigee: | 258.5535° |
| revolutions per day: | 14.96612362 |
| mean anomaly at epoch: | 101.4911° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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