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 25394U 98043A 19082.82031986 -.00000062 00000-0 -78794-5 0 9994
2 25394 98.6299 22.5654 0000794 171.0973 189.0220 14.24443102 76112
| Epoch (UTC): | 23 March 2019 19:41:15 |
| Eccentricity: | 0.0000794 |
| inclination: | 98.6299° |
| perigee height: | 810 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 22.5654° |
| argument of perigee: | 171.0973° |
| revolutions per day: | 14.24443102 |
| mean anomaly at epoch: | 189.0220° |
| orbit number at epoch: | 7611 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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