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 40906U 15049H 24340.58865164 .00133004 00000-0 11588-2 0 9990
2 40906 97.4563 4.2638 0006142 55.4490 304.7350 15.68573253511068
Epoch (UTC): | 05 December 2024 14:07:39 |
Eccentricity: | 0.0006142 |
inclination: | 97.4563° |
perigee height: | 359 km |
apogee height: | 367 km |
right ascension of ascending node: | 4.2638° |
argument of perigee: | 55.4490° |
revolutions per day: | 15.68573253 |
mean anomaly at epoch: | 304.7350° |
orbit number at epoch: | 51106 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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