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 00117U 26129.95877256 +.00000000 +00000-0 +45762-4 0 00009
2 00117 66.8109 98.3426 0081970 320.7342 38.7809 13.90186843 07
| Epoch (UTC): | 09 May 2026 23:00:37 |
| Eccentricity: | 0.0081970 |
| inclination: | 66.8109° |
| perigee height: | 868 km |
| apogee height: | 988 km |
| right ascension of ascending node: | 98.3426° |
| argument of perigee: | 320.7342° |
| revolutions per day: | 13.90186843 |
| mean anomaly at epoch: | 38.7809° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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