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 00012U 59001B 24254.48469651 .00003868 00000-0 22392-2 0 9993
2 00012 32.9131 335.0299 1654352 294.3717 49.3177 11.47077123457228
Epoch (UTC): | 10 September 2024 11:37:57 |
Eccentricity: | 0.1654352 |
inclination: | 32.9131° |
perigee height: | 553 km |
apogee height: | 3301 km |
right ascension of ascending node: | 335.0299° |
argument of perigee: | 294.3717° |
revolutions per day: | 11.47077123 |
mean anomaly at epoch: | 49.3177° |
orbit number at epoch: | 45722 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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