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 59371U 26145.59926426 +.00000000 +00000-0 +91741-4 0 00005
2 59371 97.2739 93.8956 0000674 87.3519 272.7800 15.31980769 09
| Epoch (UTC): | 25 May 2026 14:22:56 |
| Eccentricity: | 0.0000674 |
| inclination: | 97.2739° |
| perigee height: | 469 km |
| apogee height: | 470 km |
| right ascension of ascending node: | 93.8956° |
| argument of perigee: | 87.3519° |
| revolutions per day: | 15.31980769 |
| mean anomaly at epoch: | 272.7800° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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