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 14453U 83109B 22222.40570633 .00000062 00000-0 19790-4 0 9994
2 14453 81.1673 14.6357 0105076 24.3340 336.2748 14.24803726 15170
| Epoch (UTC): | 10 August 2022 09:44:13 |
| Eccentricity: | 0.0105076 |
| inclination: | 81.1673° |
| perigee height: | 733 km |
| apogee height: | 884 km |
| right ascension of ascending node: | 14.6357° |
| argument of perigee: | 24.3340° |
| revolutions per day: | 14.24803726 |
| mean anomaly at epoch: | 336.2748° |
| orbit number at epoch: | 1517 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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