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 22145.56274514 .00003065 00000-0 18135-3 0 9995
2 12586 97.6831 139.7885 0019657 130.8388 229.4550 15.12062727224602
| Epoch (UTC): | 25 May 2022 13:30:21 |
| Eccentricity: | 0.0019657 |
| inclination: | 97.6831° |
| perigee height: | 516 km |
| apogee height: | 543 km |
| right ascension of ascending node: | 139.7885° |
| argument of perigee: | 130.8388° |
| revolutions per day: | 15.12062727 |
| mean anomaly at epoch: | 229.4550° |
| orbit number at epoch: | 22460 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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