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 17973U 26066.13740324 +.00000000 +00000-0 -53473-4 0 00001
2 17973 70.8997 39.5581 0029853 21.5976 338.6397 14.14552672 03
| Epoch (UTC): | 07 March 2026 03:17:51 |
| Eccentricity: | 0.0029853 |
| inclination: | 70.8997° |
| perigee height: | 822 km |
| apogee height: | 865 km |
| right ascension of ascending node: | 39.5581° |
| argument of perigee: | 21.5976° |
| revolutions per day: | 14.14552672 |
| mean anomaly at epoch: | 338.6397° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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