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 59705U 26144.19747439 +.00000000 +00000-0 +00000-0 0 00000
2 59705 53.1260 171.5702 0026891 205.5771 154.3434 2.00564254 03
| Epoch (UTC): | 24 May 2026 04:44:21 |
| Eccentricity: | 0.0026891 |
| inclination: | 53.1260° |
| perigee height: | 20111 km |
| apogee height: | 20254 km |
| right ascension of ascending node: | 171.5702° |
| argument of perigee: | 205.5771° |
| revolutions per day: | 2.00564254 |
| mean anomaly at epoch: | 154.3434° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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