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 11963U 80073B 22142.85868011 .00000200 00000-0 10383-3 0 9996
2 11963 81.2750 178.9610 0074563 21.9190 338.5141 14.09755639143961
| Epoch (UTC): | 22 May 2022 20:36:29 |
| Eccentricity: | 0.0074563 |
| inclination: | 81.2750° |
| perigee height: | 806 km |
| apogee height: | 914 km |
| right ascension of ascending node: | 178.9610° |
| argument of perigee: | 21.9190° |
| revolutions per day: | 14.09755639 |
| mean anomaly at epoch: | 338.5141° |
| orbit number at epoch: | 14396 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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