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 50316U 82092AAH 22222.41732141 .00024912 00000-0 81298-3 0 9998
2 50316 82.5180 216.7998 0058574 242.1547 117.3752 15.29944692 36968
| Epoch (UTC): | 10 August 2022 10:00:56 |
| Eccentricity: | 0.0058574 |
| inclination: | 82.5180° |
| perigee height: | 436 km |
| apogee height: | 516 km |
| right ascension of ascending node: | 216.7998° |
| argument of perigee: | 242.1547° |
| revolutions per day: | 15.29944692 |
| mean anomaly at epoch: | 117.3752° |
| orbit number at epoch: | 3696 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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