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 23155.50827615 .00078957 00000-0 78375-3 0 9991
2 39026 97.2781 152.5137 0011642 322.6146 37.4303 15.65442916583311
Epoch (UTC): | 04 June 2023 12:11:55 |
Eccentricity: | 0.0011642 |
inclination: | 97.2781° |
perigee height: | 364 km |
apogee height: | 380 km |
right ascension of ascending node: | 152.5137° |
argument of perigee: | 322.6146° |
revolutions per day: | 15.65442916 |
mean anomaly at epoch: | 37.4303° |
orbit number at epoch: | 58331 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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