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 03047U 67116A 24280.82133120 .00001689 00000-0 38366-3 0 9994
2 03047 74.0103 112.1818 0007141 70.2421 289.9512 14.56796129 8556
| Epoch (UTC): | 06 October 2024 19:42:43 |
| Eccentricity: | 0.0007141 |
| inclination: | 74.0103° |
| perigee height: | 698 km |
| apogee height: | 708 km |
| right ascension of ascending node: | 112.1818° |
| argument of perigee: | 70.2421° |
| revolutions per day: | 14.56796129 |
| mean anomaly at epoch: | 289.9512° |
| orbit number at epoch: | 855 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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