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 25119U 97084H 18267.24750495 +.00000080 +00000-0 +71889-4 0 9991
2 25119 045.0157 186.2521 0002921 067.3304 292.7853 14.38780527087145
| Epoch (UTC): | 24 September 2018 05:56:24 |
| Eccentricity: | 0.0002921 |
| inclination: | 45.0157° |
| perigee height: | 760 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 186.2521° |
| argument of perigee: | 67.3304° |
| revolutions per day: | 14.38780527 |
| mean anomaly at epoch: | 292.7853° |
| orbit number at epoch: | 8714 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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