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 24262.86723772 .00014322 00000-0 50691-3 0 9994
2 40908 97.5241 272.4213 0012392 31.6932 328.5051 15.29181803497791
Epoch (UTC): | 18 September 2024 20:48:49 |
Eccentricity: | 0.0012392 |
inclination: | 97.5241° |
perigee height: | 470 km |
apogee height: | 487 km |
right ascension of ascending node: | 272.4213° |
argument of perigee: | 31.6932° |
revolutions per day: | 15.29181803 |
mean anomaly at epoch: | 328.5051° |
orbit number at epoch: | 49779 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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