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 40069U 14037A 22136.49009306 .00000038 00000-0 36823-4 0 9996
2 40069 98.4338 155.7503 0006843 60.8611 299.3251 14.20707203407328
Epoch (UTC): | 16 May 2022 11:45:44 |
Eccentricity: | 0.0006843 |
inclination: | 98.4338° |
perigee height: | 818 km |
apogee height: | 828 km |
right ascension of ascending node: | 155.7503° |
argument of perigee: | 60.8611° |
revolutions per day: | 14.20707203 |
mean anomaly at epoch: | 299.3251° |
orbit number at epoch: | 40732 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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