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 33410U 08053C 22145.10787458 .00003167 00000-0 21709-3 0 9990
2 33410 97.8983 151.3767 0125291 269.5700 89.1165 15.00632889740896
Epoch (UTC): | 25 May 2022 02:35:20 |
Eccentricity: | 0.0125291 |
inclination: | 97.8983° |
perigee height: | 478 km |
apogee height: | 652 km |
right ascension of ascending node: | 151.3767° |
argument of perigee: | 269.5700° |
revolutions per day: | 15.00632889 |
mean anomaly at epoch: | 89.1165° |
orbit number at epoch: | 74089 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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