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 22208U 92073B 25198.48214152 .00000070 00000-0 55965-4 0 9998
2 22208 82.9200 347.5746 0035687 83.9578 335.6661 13.75393820641510
Epoch (UTC): | 17 July 2025 11:34:17 |
Eccentricity: | 0.0035687 |
inclination: | 82.9200° |
perigee height: | 954 km |
apogee height: | 1006 km |
right ascension of ascending node: | 347.5746° |
argument of perigee: | 83.9578° |
revolutions per day: | 13.75393820 |
mean anomaly at epoch: | 335.6661° |
orbit number at epoch: | 64151 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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