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 24310.47507903 .00023611 00000-0 78276-3 0 9991
2 40908 97.5215 320.6340 0010158 201.8302 158.2507 15.31223094505076
Epoch (UTC): | 05 November 2024 11:24:06 |
Eccentricity: | 0.0010158 |
inclination: | 97.5215° |
perigee height: | 465 km |
apogee height: | 479 km |
right ascension of ascending node: | 320.6340° |
argument of perigee: | 201.8302° |
revolutions per day: | 15.31223094 |
mean anomaly at epoch: | 158.2507° |
orbit number at epoch: | 50507 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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