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 35935U 09051E 24251.60826434 .00004207 00000-0 92235-3 0 9994
2 35935 98.4597 137.0784 0009257 84.2843 275.9411 14.58150721794273
Epoch (UTC): | 07 September 2024 14:35:54 |
Eccentricity: | 0.0009257 |
inclination: | 98.4597° |
perigee height: | 692 km |
apogee height: | 706 km |
right ascension of ascending node: | 137.0784° |
argument of perigee: | 84.2843° |
revolutions per day: | 14.58150721 |
mean anomaly at epoch: | 275.9411° |
orbit number at epoch: | 79427 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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