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 27609U 02058E 24357.98715942 .00000893 00000-0 13417-3 0 9994
2 27609 64.5540 205.4851 0034755 322.1150 37.7509 14.80459838187718
| Epoch (UTC): | 22 December 2024 23:41:30 |
| Eccentricity: | 0.0034755 |
| inclination: | 64.5540° |
| perigee height: | 603 km |
| apogee height: | 652 km |
| right ascension of ascending node: | 205.4851° |
| argument of perigee: | 322.1150° |
| revolutions per day: | 14.80459838 |
| mean anomaly at epoch: | 37.7509° |
| orbit number at epoch: | 18771 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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