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 18215U 87062B 23267.10156230 .00000690 00000-0 79828-4 0 9991
2 18215 82.5100 296.8496 0021283 135.5216 277.7157 14.83929877955427
Epoch (UTC): | 24 September 2023 02:26:14 |
Eccentricity: | 0.0021283 |
inclination: | 82.5100° |
perigee height: | 602 km |
apogee height: | 632 km |
right ascension of ascending node: | 296.8496° |
argument of perigee: | 135.5216° |
revolutions per day: | 14.83929877 |
mean anomaly at epoch: | 277.7157° |
orbit number at epoch: | 95542 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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