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 31797U 07030A 22248.11368757 0.00002000 00000-0 73292-4 0 05
2 31797 98.1366 199.6938 0001001 111.7244 248.2754 15.28032921 04
Epoch (UTC): | 05 September 2022 02:43:42 |
Eccentricity: | 0.0001001 |
inclination: | 98.1366° |
perigee height: | 481 km |
apogee height: | 482 km |
right ascension of ascending node: | 199.6938° |
argument of perigee: | 111.7244° |
revolutions per day: | 15.28032921 |
mean anomaly at epoch: | 248.2754° |
orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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