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 26037.80910563 +.00000000 +00000-0 +22704-1 0 00004
2 59588 97.2238 345.8632 0045469 174.1822 185.9879 13.88347007 00
| Epoch (UTC): | 06 February 2026 19:25:06 |
| Eccentricity: | 0.0045469 |
| inclination: | 97.2238° |
| perigee height: | 901 km |
| apogee height: | 968 km |
| right ascension of ascending node: | 345.8632° |
| argument of perigee: | 174.1822° |
| revolutions per day: | 13.88347007 |
| mean anomaly at epoch: | 185.9879° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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