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 40911U 15049N 24327.12055396 .12214391 26469-5 35889-3 0 9994
2 40911 97.4275 356.1976 0007819 246.3878 113.6603 16.44746485509295
| Epoch (UTC): | 22 November 2024 02:53:35 |
| Eccentricity: | 0.0007819 |
| inclination: | 97.4275° |
| perigee height: | 148 km |
| apogee height: | 158 km |
| right ascension of ascending node: | 356.1976° |
| argument of perigee: | 246.3878° |
| revolutions per day: | 16.44746485 |
| mean anomaly at epoch: | 113.6603° |
| orbit number at epoch: | 50929 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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