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 12586U 81065B 22143.90832398 .00003208 00000-0 18969-3 0 9995
2 12586 97.6836 138.1239 0019557 135.9438 224.3354 15.12051768224355
| Epoch (UTC): | 23 May 2022 21:47:59 |
| Eccentricity: | 0.0019557 |
| inclination: | 97.6836° |
| perigee height: | 516 km |
| apogee height: | 543 km |
| right ascension of ascending node: | 138.1239° |
| argument of perigee: | 135.9438° |
| revolutions per day: | 15.12051768 |
| mean anomaly at epoch: | 224.3354° |
| orbit number at epoch: | 22435 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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