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 26104.20325618 +.00000000 +00000-0 +43249-4 0 00008
2 00117 66.8114 161.1349 0080135 337.9809 21.7833 13.90183734 01
| Epoch (UTC): | 14 April 2026 04:52:41 |
| Eccentricity: | 0.0080135 |
| inclination: | 66.8114° |
| perigee height: | 869 km |
| apogee height: | 987 km |
| right ascension of ascending node: | 161.1349° |
| argument of perigee: | 337.9809° |
| revolutions per day: | 13.90183734 |
| mean anomaly at epoch: | 21.7833° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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