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 42829U 17042E 23274.48697524 .00005074 00000-0 47719-3 0 9999
2 42829 97.3849 105.6015 0011965 223.4751 136.5528 14.94244968338365
Epoch (UTC): | 01 October 2023 11:41:14 |
Eccentricity: | 0.0011965 |
inclination: | 97.3849° |
perigee height: | 576 km |
apogee height: | 593 km |
right ascension of ascending node: | 105.6015° |
argument of perigee: | 223.4751° |
revolutions per day: | 14.94244968 |
mean anomaly at epoch: | 136.5528° |
orbit number at epoch: | 33836 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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