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 21329.71635848 0.00000000 00000-0 00000-0 0 03
2 21949 85.0101 313.7080 0003624 73.1687 286.8312 14.31496383 03
| Epoch (UTC): | 25 November 2021 17:11:33 |
| Eccentricity: | 0.0003624 |
| inclination: | 85.0101° |
| perigee height: | 784 km |
| apogee height: | 789 km |
| right ascension of ascending node: | 313.7080° |
| argument of perigee: | 73.1687° |
| revolutions per day: | 14.31496383 |
| mean anomaly at epoch: | 286.8312° |
| 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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