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 00115U 60002D 23269.38213718 .00004592 00000-0 52700-3 0 9997
2 00115 48.1637 275.3066 0031658 128.1020 232.2756 14.87037074369493
Epoch (UTC): | 26 September 2023 09:10:16 |
Eccentricity: | 0.0031658 |
inclination: | 48.1637° |
perigee height: | 585 km |
apogee height: | 629 km |
right ascension of ascending node: | 275.3066° |
argument of perigee: | 128.1020° |
revolutions per day: | 14.87037074 |
mean anomaly at epoch: | 232.2756° |
orbit number at epoch: | 36949 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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