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 59538U 26144.66457494 +.00000000 +00000-0 +31607-2 0 00004
2 59538 42.9733 219.7081 0016152 29.5667 330.6130 16.26500060 00
| Epoch (UTC): | 24 May 2026 15:56:59 |
| Eccentricity: | 0.0016152 |
| inclination: | 42.9733° |
| perigee height: | 191 km |
| apogee height: | 213 km |
| right ascension of ascending node: | 219.7081° |
| argument of perigee: | 29.5667° |
| revolutions per day: | 16.26500060 |
| mean anomaly at epoch: | 330.6130° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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