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 24252.69280146 .00004960 00000-0 67441-3 0 9992
2 27607 64.5566 324.7747 0026237 65.7659 294.6183 14.79597826168880
| Epoch (UTC): | 08 September 2024 16:37:38 |
| Eccentricity: | 0.0026237 |
| inclination: | 64.5566° |
| perigee height: | 612 km |
| apogee height: | 649 km |
| right ascension of ascending node: | 324.7747° |
| argument of perigee: | 65.7659° |
| revolutions per day: | 14.79597826 |
| mean anomaly at epoch: | 294.6183° |
| orbit number at epoch: | 16888 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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