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 23331.91989705 .00009845 00000-0 43002-3 0 9998
2 40908 97.5269 334.8183 0012841 347.8643 12.2282 15.22249066452681
Epoch (UTC): | 27 November 2023 22:04:39 |
Eccentricity: | 0.0012841 |
inclination: | 97.5269° |
perigee height: | 490 km |
apogee height: | 508 km |
right ascension of ascending node: | 334.8183° |
argument of perigee: | 347.8643° |
revolutions per day: | 15.22249066 |
mean anomaly at epoch: | 12.2282° |
orbit number at epoch: | 45268 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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