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 18145.82208276 .00000004 00000-0 16551-4 0 9990
2 25940 98.5271 85.9222 0006218 68.6123 291.5725 14.35431051974980
| Epoch (UTC): | 25 May 2018 19:43:47 |
| Eccentricity: | 0.0006218 |
| inclination: | 98.5271° |
| perigee height: | 769 km |
| apogee height: | 778 km |
| right ascension of ascending node: | 85.9222° |
| argument of perigee: | 68.6123° |
| revolutions per day: | 14.35431051 |
| mean anomaly at epoch: | 291.5725° |
| orbit number at epoch: | 97498 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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