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 23271.92313254 .00000644 00000-0 16947-3 0 9990
2 36089 98.3207 235.0358 0080112 197.8184 162.0198 14.50536668734222
Epoch (UTC): | 28 September 2023 22:09:18 |
Eccentricity: | 0.0080112 |
inclination: | 98.3207° |
perigee height: | 667 km |
apogee height: | 781 km |
right ascension of ascending node: | 235.0358° |
argument of perigee: | 197.8184° |
revolutions per day: | 14.50536668 |
mean anomaly at epoch: | 162.0198° |
orbit number at epoch: | 73422 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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