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 40907U 15049J 23332.84361188 .00030664 00000-0 89763-3 0 9996
2 40907 97.4873 342.2099 0007077 300.7068 59.3477 15.35163931453682
Epoch (UTC): | 28 November 2023 20:14:48 |
Eccentricity: | 0.0007077 |
inclination: | 97.4873° |
perigee height: | 455 km |
apogee height: | 465 km |
right ascension of ascending node: | 342.2099° |
argument of perigee: | 300.7068° |
revolutions per day: | 15.35163931 |
mean anomaly at epoch: | 59.3477° |
orbit number at epoch: | 45368 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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