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 06393U 73015B 25193.68689186 .00000084 00000-0 44048-4 0 9995
2 06393 81.2572 346.6662 0057419 275.4862 83.9759 14.05376744680647
| Epoch (UTC): | 12 July 2025 16:29:07 |
| Eccentricity: | 0.0057419 |
| inclination: | 81.2572° |
| perigee height: | 833 km |
| apogee height: | 917 km |
| right ascension of ascending node: | 346.6662° |
| argument of perigee: | 275.4862° |
| revolutions per day: | 14.05376744 |
| mean anomaly at epoch: | 83.9759° |
| orbit number at epoch: | 68064 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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