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 17912U 26161.59482007 +.00000000 +00000-0 +32063-4 0 00002
2 17912 82.5012 209.2817 0018328 213.6649 146.3405 14.85441334 02
| Epoch (UTC): | 10 June 2026 14:16:32 |
| Eccentricity: | 0.0018328 |
| inclination: | 82.5012° |
| perigee height: | 599 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 209.2817° |
| argument of perigee: | 213.6649° |
| revolutions per day: | 14.85441334 |
| mean anomaly at epoch: | 146.3405° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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