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 10096U 77055B 22144.80792521 .00000563 00000-0 61159-4 0 9997
2 10096 75.8363 37.1865 0042875 293.2821 66.3859 14.88945396430273
Epoch (UTC): | 24 May 2022 19:23:24 |
Eccentricity: | 0.0042875 |
inclination: | 75.8363° |
perigee height: | 571 km |
apogee height: | 631 km |
right ascension of ascending node: | 37.1865° |
argument of perigee: | 293.2821° |
revolutions per day: | 14.88945396 |
mean anomaly at epoch: | 66.3859° |
orbit number at epoch: | 43027 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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