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 26071.59399837 +.00000000 +00000-0 +19768-1 0 00009
2 59588 97.2052 12.0527 0062157 69.5403 291.2419 13.89752308 01
| Epoch (UTC): | 12 March 2026 14:15:21 |
| Eccentricity: | 0.0062157 |
| inclination: | 97.2052° |
| perigee height: | 884 km |
| apogee height: | 975 km |
| right ascension of ascending node: | 12.0527° |
| argument of perigee: | 69.5403° |
| revolutions per day: | 13.89752308 |
| mean anomaly at epoch: | 291.2419° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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