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 39091U 26110.32702032 +.00000000 +00000-0 +50449-4 0 00000
2 39091 98.3982 291.1980 0011183 57.1021 303.1240 14.36517961 09
| Epoch (UTC): | 20 April 2026 07:50:54 |
| Eccentricity: | 0.0011183 |
| inclination: | 98.3982° |
| perigee height: | 762 km |
| apogee height: | 778 km |
| right ascension of ascending node: | 291.1980° |
| argument of perigee: | 57.1021° |
| revolutions per day: | 14.36517961 |
| mean anomaly at epoch: | 303.1240° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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