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 34116U 93036KM 23080.52035044 .00004124 00000-0 12338-2 0 9992
2 34116 74.0449 247.7757 0014753 207.8141 208.3062 14.43137407740553
Epoch (UTC): | 21 March 2023 12:29:18 |
Eccentricity: | 0.0014753 |
inclination: | 74.0449° |
perigee height: | 737 km |
apogee height: | 758 km |
right ascension of ascending node: | 247.7757° |
argument of perigee: | 207.8141° |
revolutions per day: | 14.43137407 |
mean anomaly at epoch: | 208.3062° |
orbit number at epoch: | 74055 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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