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 59708U 26144.88341399 +.00000000 +00000-0 +20368-4 0 00007
2 59708 53.1583 310.3572 0001062 91.7941 268.3199 15.69711221 00
| Epoch (UTC): | 24 May 2026 21:12:06 |
| Eccentricity: | 0.0001062 |
| inclination: | 53.1583° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 310.3572° |
| argument of perigee: | 91.7941° |
| revolutions per day: | 15.69711221 |
| mean anomaly at epoch: | 268.3199° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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