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 11U 59001A 23150.73002170 .00000887 00000-0 44937-3 0 9991
2 11 32.8762 328.5051 1462220 216.5378 132.6161 11.87166469744650
Epoch (UTC): | 30 May 2023 17:31:13 |
Eccentricity: | 0.1462220 |
inclination: | 32.8762° |
perigee height: | 552 km |
apogee height: | 2926 km |
right ascension of ascending node: | 328.5051° |
argument of perigee: | 216.5378° |
revolutions per day: | 11.87166469 |
mean anomaly at epoch: | 132.6161° |
orbit number at epoch: | 74465 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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