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 39026U 12072A 23078.75071066 .00063966 00000-0 10112-2 0 9991
2 39026 97.2824 73.8863 0017670 233.3047 126.6584 15.53083882571358
Epoch (UTC): | 19 March 2023 18:01:01 |
Eccentricity: | 0.0017670 |
inclination: | 97.2824° |
perigee height: | 396 km |
apogee height: | 420 km |
right ascension of ascending node: | 73.8863° |
argument of perigee: | 233.3047° |
revolutions per day: | 15.53083882 |
mean anomaly at epoch: | 126.6584° |
orbit number at epoch: | 57135 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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