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 data is extracted from the following two-line orbital elements,
1 25396U 98043C 19081.77840207 +.00000005 +00000-0 +20960-4 0 9999
2 25396 098.6581 023.8039 0001540 246.6944 113.4073 14.24509196075545
| Epoch (UTC): | 22 March 2019 18:40:53 |
| Eccentricity: | 0.0001540 |
| inclination: | 98.6581° |
| perigee height: | 809 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 23.8039° |
| argument of perigee: | 246.6944° |
| revolutions per day: | 14.24509196 |
| mean anomaly at epoch: | 113.4073° |
| orbit number at epoch: | 7554 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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