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 23275.69485985 .00000278 00000-0 16286-3 0 9993
2 06393 81.2530 252.5724 0057821 299.0683 60.4701 14.05156724589497
| Epoch (UTC): | 02 October 2023 16:40:35 |
| Eccentricity: | 0.0057821 |
| inclination: | 81.2530° |
| perigee height: | 834 km |
| apogee height: | 918 km |
| right ascension of ascending node: | 252.5724° |
| argument of perigee: | 299.0683° |
| revolutions per day: | 14.05156724 |
| mean anomaly at epoch: | 60.4701° |
| orbit number at epoch: | 58949 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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