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 00045U 60007A 23275.81918435 .00001229 00000-0 33211-3 0 9997
2 00045 66.6929 91.3630 0251490 161.8514 199.1770 14.34339309238217
Epoch (UTC): | 02 October 2023 19:39:37 |
Eccentricity: | 0.0251490 |
inclination: | 66.6929° |
perigee height: | 597 km |
apogee height: | 957 km |
right ascension of ascending node: | 91.3630° |
argument of perigee: | 161.8514° |
revolutions per day: | 14.34339309 |
mean anomaly at epoch: | 199.1770° |
orbit number at epoch: | 23821 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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