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 23086.86017207 .00001568 00000-0 36339-3 0 9997
2 35935 98.5366 316.6298 0006827 275.8007 84.2412 14.56502190717123
Epoch (UTC): | 27 March 2023 20:38:38 |
Eccentricity: | 0.0006827 |
inclination: | 98.5366° |
perigee height: | 699 km |
apogee height: | 709 km |
right ascension of ascending node: | 316.6298° |
argument of perigee: | 275.8007° |
revolutions per day: | 14.56502190 |
mean anomaly at epoch: | 84.2412° |
orbit number at epoch: | 71712 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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