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 37766U 11039B 25198.29421131 .00000459 00000-0 84755-4 0 9992
2 37766 98.1379 92.5219 0041922 295.2356 64.4507 14.69730919747593
| Epoch (UTC): | 17 July 2025 07:03:39 |
| Eccentricity: | 0.0041922 |
| inclination: | 98.1379° |
| perigee height: | 632 km |
| apogee height: | 691 km |
| right ascension of ascending node: | 92.5219° |
| argument of perigee: | 295.2356° |
| revolutions per day: | 14.69730919 |
| mean anomaly at epoch: | 64.4507° |
| orbit number at epoch: | 74759 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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