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 23152.52078773 -.00000056 00000-0 -40793-5 0 9994
2 22803 70.9903 345.0928 0018901 307.8896 52.0517 14.16934061536140
Epoch (UTC): | 01 June 2023 12:29:56 |
Eccentricity: | 0.0018901 |
inclination: | 70.9903° |
perigee height: | 822 km |
apogee height: | 849 km |
right ascension of ascending node: | 345.0928° |
argument of perigee: | 307.8896° |
revolutions per day: | 14.16934061 |
mean anomaly at epoch: | 52.0517° |
orbit number at epoch: | 53614 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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