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 40908U 15049K 24263.52159735 .00015488 00000-0 54754-3 0 9998
2 40908 97.5241 273.0832 0012306 29.3986 330.7943 15.29202045497891
| Epoch (UTC): | 19 September 2024 12:31:06 |
| Eccentricity: | 0.0012306 |
| inclination: | 97.5241° |
| perigee height: | 470 km |
| apogee height: | 486 km |
| right ascension of ascending node: | 273.0832° |
| argument of perigee: | 29.3986° |
| revolutions per day: | 15.29202045 |
| mean anomaly at epoch: | 330.7943° |
| orbit number at epoch: | 49789 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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