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 22826U 93061D 22136.08354826 .00000136 00000-0 69932-4 0 9992
2 22826 98.8840 166.3139 0009884 128.7023 231.5044 14.30511322494031
Epoch (UTC): | 16 May 2022 02:00:18 |
Eccentricity: | 0.0009884 |
inclination: | 98.8840° |
perigee height: | 783 km |
apogee height: | 797 km |
right ascension of ascending node: | 166.3139° |
argument of perigee: | 128.7023° |
revolutions per day: | 14.30511322 |
mean anomaly at epoch: | 231.5044° |
orbit number at epoch: | 49403 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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