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 42790U 17036AB 23088.64021097 .00177470 00000-0 20659-2 0 9999
2 42790 97.1541 135.1231 0002226 11.1767 348.9540 15.61104925321184
Epoch (UTC): | 29 March 2023 15:21:54 |
Eccentricity: | 0.0002226 |
inclination: | 97.1541° |
perigee height: | 383 km |
apogee height: | 386 km |
right ascension of ascending node: | 135.1231° |
argument of perigee: | 11.1767° |
revolutions per day: | 15.61104925 |
mean anomaly at epoch: | 348.9540° |
orbit number at epoch: | 32118 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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