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 26073.82579830 +.00000000 +00000-0 +26159-1 0 00002
2 59588 97.2035 13.7831 0064398 64.3072 296.4724 13.89878315 05
| Epoch (UTC): | 14 March 2026 19:49:08 |
| Eccentricity: | 0.0064398 |
| inclination: | 97.2035° |
| perigee height: | 882 km |
| apogee height: | 976 km |
| right ascension of ascending node: | 13.7831° |
| argument of perigee: | 64.3072° |
| revolutions per day: | 13.89878315 |
| mean anomaly at epoch: | 296.4724° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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