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 21064.79189785 0.00000020 00000-0 75425-5 0 01
2 21949 85.0126 106.3720 0005695 91.6555 268.3443 14.31471407 06
| Epoch (UTC): | 05 March 2021 19:00:19 |
| Eccentricity: | 0.0005695 |
| inclination: | 85.0126° |
| perigee height: | 783 km |
| apogee height: | 791 km |
| right ascension of ascending node: | 106.3720° |
| argument of perigee: | 91.6555° |
| revolutions per day: | 14.31471407 |
| mean anomaly at epoch: | 268.3443° |
| 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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