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 23027.07478327 .00001070 00000-0 29012-3 0 9999
2 45 66.6946 27.4812 0257185 339.8478 19.2607 14.34025562259410
Epoch (UTC): | 27 January 2023 01:47:41 |
Eccentricity: | 0.0257185 |
inclination: | 66.6946° |
perigee height: | 594 km |
apogee height: | 962 km |
right ascension of ascending node: | 27.4812° |
argument of perigee: | 339.8478° |
revolutions per day: | 14.34025562 |
mean anomaly at epoch: | 19.2607° |
orbit number at epoch: | 25941 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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