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 07411U 74063A 22228.45679018 .00000136 00000-0 71741-4 0 9993
2 07411 98.6366 72.9365 0042064 157.1527 203.1537 14.28129395494337
Epoch (UTC): | 16 August 2022 10:57:46 |
Eccentricity: | 0.0042064 |
inclination: | 98.6366° |
perigee height: | 768 km |
apogee height: | 828 km |
right ascension of ascending node: | 72.9365° |
argument of perigee: | 157.1527° |
revolutions per day: | 14.28129395 |
mean anomaly at epoch: | 203.1537° |
orbit number at epoch: | 49433 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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