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 36796U 10035B 25189.75677319 .00002945 00000-0 23519-3 0 9993
2 36796 98.1315 75.6884 0010893 81.6870 278.5588 15.01065571813566
| Epoch (UTC): | 08 July 2025 18:09:45 |
| Eccentricity: | 0.0010893 |
| inclination: | 98.1315° |
| perigee height: | 556 km |
| apogee height: | 571 km |
| right ascension of ascending node: | 75.6884° |
| argument of perigee: | 81.6870° |
| revolutions per day: | 15.01065571 |
| mean anomaly at epoch: | 278.5588° |
| orbit number at epoch: | 81356 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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