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 9903U 77024A 23160.86402037 .00000212 00000-0 11599-3 0 9996
2 9903 81.2714 125.3768 0036376 242.6106 117.1362 14.08470521372436
Epoch (UTC): | 09 June 2023 20:44:11 |
Eccentricity: | 0.0036376 |
inclination: | 81.2714° |
perigee height: | 838 km |
apogee height: | 891 km |
right ascension of ascending node: | 125.3768° |
argument of perigee: | 242.6106° |
revolutions per day: | 14.08470521 |
mean anomaly at epoch: | 117.1362° |
orbit number at epoch: | 37243 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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