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 06155U 72065B 24357.50306948 .00002643 00000-0 37832-3 0 9994
2 06155 35.0039 13.8666 0035748 252.4802 107.1990 14.75833250775856
| Epoch (UTC): | 22 December 2024 12:04:25 |
| Eccentricity: | 0.0035748 |
| inclination: | 35.0039° |
| perigee height: | 617 km |
| apogee height: | 667 km |
| right ascension of ascending node: | 13.8666° |
| argument of perigee: | 252.4802° |
| revolutions per day: | 14.75833250 |
| mean anomaly at epoch: | 107.1990° |
| orbit number at epoch: | 77585 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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