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 25984U 99065E 21023.59960556 -.00000156 00000-0 -53352-5 0 9997
2 25984 45.0402 96.3183 0005316 211.8138 148.2388 14.32976512103967
Epoch (UTC): | 23 January 2021 14:23:25 |
Eccentricity: | 0.0005316 |
inclination: | 45.0402° |
perigee height: | 778 km |
apogee height: | 785 km |
right ascension of ascending node: | 96.3183° |
argument of perigee: | 211.8138° |
revolutions per day: | 14.32976512 |
mean anomaly at epoch: | 148.2388° |
orbit number at epoch: | 10396 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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