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 24318.16519016 .00000293 00000-0 16893-3 0 9992
2 22803 70.9895 306.4780 0018928 229.2597 130.6884 14.17103576611572
Epoch (UTC): | 13 November 2024 03:57:52 |
Eccentricity: | 0.0018928 |
inclination: | 70.9895° |
perigee height: | 821 km |
apogee height: | 849 km |
right ascension of ascending node: | 306.4780° |
argument of perigee: | 229.2597° |
revolutions per day: | 14.17103576 |
mean anomaly at epoch: | 130.6884° |
orbit number at epoch: | 61157 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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