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 11416U 79057A 23089.02270309 .00000708 00000-0 26937-3 0 9991
2 11416 98.6575 105.2464 0011229 131.8279 228.3865 14.33988209282657
Epoch (UTC): | 30 March 2023 00:32:41 |
Eccentricity: | 0.0011229 |
inclination: | 98.6575° |
perigee height: | 770 km |
apogee height: | 786 km |
right ascension of ascending node: | 105.2464° |
argument of perigee: | 131.8279° |
revolutions per day: | 14.33988209 |
mean anomaly at epoch: | 228.3865° |
orbit number at epoch: | 28265 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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