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 24357.48767365 .00003002 00000-0 40481-3 0 9999
2 27607 64.5554 2.0902 0035967 19.8856 340.3641 14.80550973184188
| Epoch (UTC): | 22 December 2024 11:42:15 |
| Eccentricity: | 0.0035967 |
| inclination: | 64.5554° |
| perigee height: | 602 km |
| apogee height: | 653 km |
| right ascension of ascending node: | 2.0902° |
| argument of perigee: | 19.8856° |
| revolutions per day: | 14.80550973 |
| mean anomaly at epoch: | 340.3641° |
| orbit number at epoch: | 18418 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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