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 19650U 88102B 25199.53453796 -.00000103 00000-0 -28107-4 0 9996
2 19650 71.0003 284.1632 0014254 357.9155 2.1906 14.16110564893749
| Epoch (UTC): | 18 July 2025 12:49:44 |
| Eccentricity: | 0.0014254 |
| inclination: | 71.0003° |
| perigee height: | 828 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 284.1632° |
| argument of perigee: | 357.9155° |
| revolutions per day: | 14.16110564 |
| mean anomaly at epoch: | 2.1906° |
| orbit number at epoch: | 89374 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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