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 33493U 09002B 23091.76185998 .00015447 00000-0 10986-2 0 9998
2 33493 98.2512 101.0127 0014897 306.1186 53.8659 15.04676818772241
Epoch (UTC): | 01 April 2023 18:17:04 |
Eccentricity: | 0.0014897 |
inclination: | 98.2512° |
perigee height: | 542 km |
apogee height: | 563 km |
right ascension of ascending node: | 101.0127° |
argument of perigee: | 306.1186° |
revolutions per day: | 15.04676818 |
mean anomaly at epoch: | 53.8659° |
orbit number at epoch: | 77224 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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