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 17290U 26088.18300918 +.00000000 +00000-0 +21671-4 0 00007
2 17290 82.4693 160.2415 0013815 43.3207 316.9037 13.85263684 04
| Epoch (UTC): | 29 March 2026 04:23:31 |
| Eccentricity: | 0.0013815 |
| inclination: | 82.4693° |
| perigee height: | 935 km |
| apogee height: | 955 km |
| right ascension of ascending node: | 160.2415° |
| argument of perigee: | 43.3207° |
| revolutions per day: | 13.85263684 |
| mean anomaly at epoch: | 316.9037° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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