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 00046U 60007B 24311.59869897 .00003312 00000-0 64079-3 0 9993
2 00046 66.6920 28.2336 0198170 12.3469 348.2392 14.52907703371578
Epoch (UTC): | 06 November 2024 14:22:07 |
Eccentricity: | 0.0198170 |
inclination: | 66.6920° |
perigee height: | 575 km |
apogee height: | 857 km |
right ascension of ascending node: | 28.2336° |
argument of perigee: | 12.3469° |
revolutions per day: | 14.52907703 |
mean anomaly at epoch: | 348.2392° |
orbit number at epoch: | 37157 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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