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 23033.29432716 .00001316 00000-0 19855-3 0 9994
2 27607 64.5558 318.3170 0078822 250.8881 108.3676 14.76687424 82302
| Epoch (UTC): | 02 February 2023 07:03:49 |
| Eccentricity: | 0.0078822 |
| inclination: | 64.5558° |
| perigee height: | 584 km |
| apogee height: | 695 km |
| right ascension of ascending node: | 318.3170° |
| argument of perigee: | 250.8881° |
| revolutions per day: | 14.76687424 |
| mean anomaly at epoch: | 108.3676° |
| orbit number at epoch: | 8230 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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