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 26159.30437500 +.00000000 +00000-0 +20019-1 0 00006
2 59588 97.1681 80.0763 0051344 68.3061 292.3561 13.93888153 01
| Epoch (UTC): | 08 June 2026 07:18:18 |
| Eccentricity: | 0.0051344 |
| inclination: | 97.1681° |
| perigee height: | 878 km |
| apogee height: | 952 km |
| right ascension of ascending node: | 80.0763° |
| argument of perigee: | 68.3061° |
| revolutions per day: | 13.93888153 |
| mean anomaly at epoch: | 292.3561° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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