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 36582U 10021B 25166.86499527 .00000100 00000-0 00000-0 0 9999
2 36582 0.0697 75.0044 0002203 15.6436 138.3719 1.00268897 55283
| Epoch (UTC): | 15 June 2025 20:45:35 |
| Eccentricity: | 0.0002203 |
| inclination: | 0.0697° |
| perigee height: | 35778 km |
| apogee height: | 35796 km |
| right ascension of ascending node: | 75.0044° |
| argument of perigee: | 15.6436° |
| revolutions per day: | 1.00268897 |
| mean anomaly at epoch: | 138.3719° |
| orbit number at epoch: | 5528 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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