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 28415U 04035C 24357.67843246 .00009887 00000-0 44749-3 0 9996
2 28415 97.4031 27.5134 0040675 86.8570 273.7318 15.20338779112554
| Epoch (UTC): | 22 December 2024 16:16:56 |
| Eccentricity: | 0.0040675 |
| inclination: | 97.4031° |
| perigee height: | 477 km |
| apogee height: | 533 km |
| right ascension of ascending node: | 27.5134° |
| argument of perigee: | 86.8570° |
| revolutions per day: | 15.20338779 |
| mean anomaly at epoch: | 273.7318° |
| orbit number at epoch: | 11255 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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