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 36089U 09061B 23150.16582851 .00000261 00000-0 76034-4 0 9992
2 36089 98.3068 114.8020 0080152 210.2961 149.3588 14.50387389716577
Epoch (UTC): | 30 May 2023 03:58:47 |
Eccentricity: | 0.0080152 |
inclination: | 98.3068° |
perigee height: | 667 km |
apogee height: | 781 km |
right ascension of ascending node: | 114.8020° |
argument of perigee: | 210.2961° |
revolutions per day: | 14.50387389 |
mean anomaly at epoch: | 149.3588° |
orbit number at epoch: | 71657 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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