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 21949U 92023A 20335.72578344 0.00000000 00000-0 00000-0 0 07
2 21949 85.0126 161.1457 0005695 34.6522 325.3476 14.31465060 01
| Epoch (UTC): | 30 November 2020 17:25:07 |
| Eccentricity: | 0.0005695 |
| inclination: | 85.0126° |
| perigee height: | 783 km |
| apogee height: | 791 km |
| right ascension of ascending node: | 161.1457° |
| argument of perigee: | 34.6522° |
| revolutions per day: | 14.31465060 |
| mean anomaly at epoch: | 325.3476° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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