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 23087.13531953 .00023954 00000-0 93816-3 0 9992
2 40907 97.4962 94.4555 0013996 84.1438 341.5378 15.25702753416118
Epoch (UTC): | 28 March 2023 03:14:51 |
Eccentricity: | 0.0013996 |
inclination: | 97.4962° |
perigee height: | 479 km |
apogee height: | 498 km |
right ascension of ascending node: | 94.4555° |
argument of perigee: | 84.1438° |
revolutions per day: | 15.25702753 |
mean anomaly at epoch: | 341.5378° |
orbit number at epoch: | 41611 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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