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 is defined by the following mean orbital elements,
1 63919U 26145.61145321 +.00000000 +00000-0 +53972-4 0 00002
2 63919 85.9962 198.0526 0002046 101.0507 259.0907 14.12443865 06
| Epoch (UTC): | 25 May 2026 14:40:29 |
| Eccentricity: | 0.0002046 |
| inclination: | 85.9962° |
| perigee height: | 850 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 198.0526° |
| argument of perigee: | 101.0507° |
| revolutions per day: | 14.12443865 |
| mean anomaly at epoch: | 259.0907° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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