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 26389U 00034B 25196.57598301 .00023052 00000-0 12687-2 0 9994
2 26389 26.9065 66.0674 4973017 216.6180 96.0523 5.74125396398302
| Epoch (UTC): | 15 July 2025 13:49:24 |
| Eccentricity: | 0.4973017 |
| inclination: | 26.9065° |
| perigee height: | 244 km |
| apogee height: | 13348 km |
| right ascension of ascending node: | 66.0674° |
| argument of perigee: | 216.6180° |
| revolutions per day: | 5.74125396 |
| mean anomaly at epoch: | 96.0523° |
| orbit number at epoch: | 39830 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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