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 17974U 26075.86889844 +.00000000 +00000-0 +67483-4 0 00008
2 17974 71.0105 17.6910 0014630 202.8641 218.9500 14.17644734 01
| Epoch (UTC): | 16 March 2026 20:51:12 |
| Eccentricity: | 0.0014630 |
| inclination: | 71.0105° |
| perigee height: | 823 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 17.6910° |
| argument of perigee: | 202.8641° |
| revolutions per day: | 14.17644734 |
| mean anomaly at epoch: | 218.9500° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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