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 22176.59980501 .00000112 00000-0 64082-4 0 9991
2 00012 32.9025 287.8617 1665096 357.4887 1.8112 11.44680565364556
Epoch (UTC): | 25 June 2022 14:23:43 |
Eccentricity: | 0.1665096 |
inclination: | 32.9025° |
perigee height: | 553 km |
apogee height: | 3323 km |
right ascension of ascending node: | 287.8617° |
argument of perigee: | 357.4887° |
revolutions per day: | 11.44680565 |
mean anomaly at epoch: | 1.8112° |
orbit number at epoch: | 36455 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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