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 29897U 99025GT 24358.23401692 .00005363 00000-0 57730-2 0 9990
2 29897 98.6414 259.5162 0307221 339.7422 174.8740 13.55222291881453
Epoch (UTC): | 23 December 2024 05:36:59 |
Eccentricity: | 0.0307221 |
inclination: | 98.6414° |
perigee height: | 825 km |
apogee height: | 1281 km |
right ascension of ascending node: | 259.5162° |
argument of perigee: | 339.7422° |
revolutions per day: | 13.55222291 |
mean anomaly at epoch: | 174.8740° |
orbit number at epoch: | 88145 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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