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 23277.47852872 .00002516 00000-0 36044-3 0 9995
2 27607 64.5545 289.7799 0057028 201.3972 158.4748 14.77703576118374
| Epoch (UTC): | 04 October 2023 11:29:04 |
| Eccentricity: | 0.0057028 |
| inclination: | 64.5545° |
| perigee height: | 596 km |
| apogee height: | 676 km |
| right ascension of ascending node: | 289.7799° |
| argument of perigee: | 201.3972° |
| revolutions per day: | 14.77703576 |
| mean anomaly at epoch: | 158.4748° |
| orbit number at epoch: | 11837 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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