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 20150U 89059B 21110.57235306 -.00000059 00000-0 -76258-4 0 9993
2 20150 82.9373 133.0131 0028128 326.1522 148.0749 13.75652847593127
| Epoch (UTC): | 20 April 2021 13:44:11 |
| Eccentricity: | 0.0028128 |
| inclination: | 82.9373° |
| perigee height: | 958 km |
| apogee height: | 1000 km |
| right ascension of ascending node: | 133.0131° |
| argument of perigee: | 326.1522° |
| revolutions per day: | 13.75652847 |
| mean anomaly at epoch: | 148.0749° |
| orbit number at epoch: | 59312 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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