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 31455U 99025BUT 22224.32418774 .00000137 00000-0 83219-4 0 9999
2 31455 98.5931 253.4436 0222351 283.2355 74.4101 14.09215211789316
Epoch (UTC): | 12 August 2022 07:46:49 |
Eccentricity: | 0.0222351 |
inclination: | 98.5931° |
perigee height: | 701 km |
apogee height: | 1023 km |
right ascension of ascending node: | 253.4436° |
argument of perigee: | 283.2355° |
revolutions per day: | 14.09215211 |
mean anomaly at epoch: | 74.4101° |
orbit number at epoch: | 78931 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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