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 22803U 93059B 23151.88542397 -.00000088 00000-0 -20064-4 0 9993
2 22803 70.9904 346.4321 0018895 308.7674 51.1761 14.16934074536054
Epoch (UTC): | 31 May 2023 21:15:00 |
Eccentricity: | 0.0018895 |
inclination: | 70.9904° |
perigee height: | 822 km |
apogee height: | 849 km |
right ascension of ascending node: | 346.4321° |
argument of perigee: | 308.7674° |
revolutions per day: | 14.16934074 |
mean anomaly at epoch: | 51.1761° |
orbit number at epoch: | 53605 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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