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 36702U 99025DZY 22311.34778288 .00009864 00000-0 34453-2 0 9997
2 36702 98.4534 347.9316 0108353 148.3092 212.4675 14.32151904490799
Epoch (UTC): | 07 November 2022 08:20:48 |
Eccentricity: | 0.0108353 |
inclination: | 98.4534° |
perigee height: | 707 km |
apogee height: | 862 km |
right ascension of ascending node: | 347.9316° |
argument of perigee: | 148.3092° |
revolutions per day: | 14.32151904 |
mean anomaly at epoch: | 212.4675° |
orbit number at epoch: | 49079 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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