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 23088.46856205 -.00000064 00000-0 00000-0 0 9992
2 25019 11.3847 29.7119 0005008 338.5301 234.7700 1.00276144 21166
| Epoch (UTC): | 29 March 2023 11:14:43 |
| Eccentricity: | 0.0005008 |
| inclination: | 11.3847° |
| perigee height: | 35764 km |
| apogee height: | 35806 km |
| right ascension of ascending node: | 29.7119° |
| argument of perigee: | 338.5301° |
| revolutions per day: | 1.00276144 |
| mean anomaly at epoch: | 234.7700° |
| orbit number at epoch: | 2116 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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