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 25940U 99057A 18262.57840713 +.00000004 +00000-0 +16668-4 0 9999
2 25940 098.5332 201.3625 0006264 079.0020 281.1870 14.35442205991711
| Epoch (UTC): | 19 September 2018 13:52:54 |
| Eccentricity: | 0.0006264 |
| inclination: | 98.5332° |
| perigee height: | 769 km |
| apogee height: | 778 km |
| right ascension of ascending node: | 201.3625° |
| argument of perigee: | 79.0020° |
| revolutions per day: | 14.35442205 |
| mean anomaly at epoch: | 281.1870° |
| orbit number at epoch: | 99171 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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