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 35868U 09049D 21015.89238460 .00000005 00000-0 20930-4 0 9994
2 35868 98.4464 1.4196 0003005 267.7559 92.3275 14.22906320588252
| Epoch (UTC): | 15 January 2021 21:25:02 |
| Eccentricity: | 0.0003005 |
| inclination: | 98.4464° |
| perigee height: | 813 km |
| apogee height: | 818 km |
| right ascension of ascending node: | 1.4196° |
| argument of perigee: | 267.7559° |
| revolutions per day: | 14.22906320 |
| mean anomaly at epoch: | 92.3275° |
| orbit number at epoch: | 58825 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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