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 6393U 73015B 23339.56639786 .00000202 00000-0 11527-3 0 9990
2 6393 81.2555 190.9931 0059394 118.7861 241.9290 14.05175765598733
| Epoch (UTC): | 05 December 2023 13:35:36 |
| Eccentricity: | 0.0059394 |
| inclination: | 81.2555° |
| perigee height: | 833 km |
| apogee height: | 919 km |
| right ascension of ascending node: | 190.9931° |
| argument of perigee: | 118.7861° |
| revolutions per day: | 14.05175765 |
| mean anomaly at epoch: | 241.9290° |
| orbit number at epoch: | 59873 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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