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 23657U 95046A 24357.67496527 .00003127 00000-0 30709-3 0 9999
2 23657 82.5242 196.9786 0019763 341.5962 18.4540 14.91741690585169
Epoch (UTC): | 22 December 2024 16:11:56 |
Eccentricity: | 0.0019763 |
inclination: | 82.5242° |
perigee height: | 579 km |
apogee height: | 606 km |
right ascension of ascending node: | 196.9786° |
argument of perigee: | 341.5962° |
revolutions per day: | 14.91741690 |
mean anomaly at epoch: | 18.4540° |
orbit number at epoch: | 58516 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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