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 45U 60007A 23160.90107131 .00000145 00000-0 61946-4 0 9996
2 45 66.6952 34.5106 0260752 244.6661 112.7228 14.34222324278608
Epoch (UTC): | 09 June 2023 21:37:32 |
Eccentricity: | 0.0260752 |
inclination: | 66.6952° |
perigee height: | 591 km |
apogee height: | 964 km |
right ascension of ascending node: | 34.5106° |
argument of perigee: | 244.6661° |
revolutions per day: | 14.34222324 |
mean anomaly at epoch: | 112.7228° |
orbit number at epoch: | 27860 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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