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 25019U 97065A 18143.75501175 0.00000000 00000-0 00000-0 0 05
2 25019 9.3269 41.2483 0006998 246.0425 113.8924 1.00270000 03
| Epoch (UTC): | 23 May 2018 18:07:13 |
| Eccentricity: | 0.0006998 |
| inclination: | 9.3269° |
| perigee height: | 35757 km |
| apogee height: | 35816 km |
| right ascension of ascending node: | 41.2483° |
| argument of perigee: | 246.0425° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 113.8924° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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