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 37162U 10046A 22208.67227616 0.00000080 00000-0 14322-3 0 07
2 37162 123.0043 207.7860 0006249 102.8484 257.1515 13.41442314 05
Epoch (UTC): | 27 July 2022 16:08:04 |
Eccentricity: | 0.0006249 |
inclination: | 123.0043° |
perigee height: | 1099 km |
apogee height: | 1108 km |
right ascension of ascending node: | 207.7860° |
argument of perigee: | 102.8484° |
revolutions per day: | 13.41442314 |
mean anomaly at epoch: | 257.1515° |
orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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