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 42941U 17056A 23058.52378684 0.00000000 00000-0 00000-0 0 03
2 42941 63.1952 277.8236 7046149 268.9863 91.0139 2.00619834 02
Epoch (UTC): | 27 February 2023 12:34:15 |
Eccentricity: | 0.7046149 |
inclination: | 63.1952° |
perigee height: | 1466 km |
apogee height: | 38888 km |
right ascension of ascending node: | 277.8236° |
argument of perigee: | 268.9863° |
revolutions per day: | 2.00619834 |
mean anomaly at epoch: | 91.0139° |
orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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