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 25136.92124524 .00000290 00000-0 80658-4 0 9990
2 36089 98.4076 107.9368 0078562 172.9956 187.2356 14.51965417820570
Epoch (UTC): | 16 May 2025 22:06:35 |
Eccentricity: | 0.0078562 |
inclination: | 98.4076° |
perigee height: | 663 km |
apogee height: | 775 km |
right ascension of ascending node: | 107.9368° |
argument of perigee: | 172.9956° |
revolutions per day: | 14.51965417 |
mean anomaly at epoch: | 187.2356° |
orbit number at epoch: | 82057 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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