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 40907U 15049J 24258.84053312 .00147735 00000-0 14354-2 0 9992
2 40907 97.4641 282.2805 0001245 345.2331 14.8893 15.65836925498647
| Epoch (UTC): | 14 September 2024 20:10:22 |
| Eccentricity: | 0.0001245 |
| inclination: | 97.4641° |
| perigee height: | 370 km |
| apogee height: | 371 km |
| right ascension of ascending node: | 282.2805° |
| argument of perigee: | 345.2331° |
| revolutions per day: | 15.65836925 |
| mean anomaly at epoch: | 14.8893° |
| orbit number at epoch: | 49864 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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