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 40906U 15049H 24278.15041369 .00103717 00000-0 15697-2 0 9999
2 40906 97.4694 298.5579 0003747 246.6481 113.4378 15.54307023501325
Epoch (UTC): | 04 October 2024 03:36:35 |
Eccentricity: | 0.0003747 |
inclination: | 97.4694° |
perigee height: | 401 km |
apogee height: | 407 km |
right ascension of ascending node: | 298.5579° |
argument of perigee: | 246.6481° |
revolutions per day: | 15.54307023 |
mean anomaly at epoch: | 113.4378° |
orbit number at epoch: | 50132 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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