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 23338.09861177 .00008440 00000-0 36772-3 0 9992
2 40908 97.5281 341.0034 0012116 324.9282 35.1156 15.22389861453627
Epoch (UTC): | 04 December 2023 02:22:00 |
Eccentricity: | 0.0012116 |
inclination: | 97.5281° |
perigee height: | 490 km |
apogee height: | 507 km |
right ascension of ascending node: | 341.0034° |
argument of perigee: | 324.9282° |
revolutions per day: | 15.22389861 |
mean anomaly at epoch: | 35.1156° |
orbit number at epoch: | 45362 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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