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 27607U 02058C 23334.59171869 .00001781 00000-0 26080-3 0 9994
2 27607 64.5569 114.5455 0049760 186.9788 173.0629 14.77982604127025
| Epoch (UTC): | 30 November 2023 14:12:04 |
| Eccentricity: | 0.0049760 |
| inclination: | 64.5569° |
| perigee height: | 601 km |
| apogee height: | 670 km |
| right ascension of ascending node: | 114.5455° |
| argument of perigee: | 186.9788° |
| revolutions per day: | 14.77982604 |
| mean anomaly at epoch: | 173.0629° |
| orbit number at epoch: | 12702 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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