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 26100.17445559 +.00000000 +00000-0 +44707-4 0 00007
2 00117 66.8122 170.9564 0079821 340.7151 19.0911 13.90183418 05
| Epoch (UTC): | 10 April 2026 04:11:12 |
| Eccentricity: | 0.0079821 |
| inclination: | 66.8122° |
| perigee height: | 870 km |
| apogee height: | 986 km |
| right ascension of ascending node: | 170.9564° |
| argument of perigee: | 340.7151° |
| revolutions per day: | 13.90183418 |
| mean anomaly at epoch: | 19.0911° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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