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 00979U 65004B 22183.86212435 .00000066 00000-0 94822-4 0 9998
2 00979 96.4120 355.0535 1142585 167.3171 195.9433 12.14761529540020
Epoch (UTC): | 02 July 2022 20:41:27 |
Eccentricity: | 0.1142585 |
inclination: | 96.4120° |
perigee height: | 702 km |
apogee height: | 2529 km |
right ascension of ascending node: | 355.0535° |
argument of perigee: | 167.3171° |
revolutions per day: | 12.14761529 |
mean anomaly at epoch: | 195.9433° |
orbit number at epoch: | 54002 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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