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 26149.09552696 +.00000000 +00000-0 +40827-4 0 00001
2 00117 66.8137 51.6893 0083020 308.1537 51.2080 13.90188656 07
| Epoch (UTC): | 29 May 2026 02:17:33 |
| Eccentricity: | 0.0083020 |
| inclination: | 66.8137° |
| perigee height: | 867 km |
| apogee height: | 989 km |
| right ascension of ascending node: | 51.6893° |
| argument of perigee: | 308.1537° |
| revolutions per day: | 13.90188656 |
| mean anomaly at epoch: | 51.2080° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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