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 00053U 60009E 22279.42011582 -.00000105 00000-0 -19412-3 0 9996
2 00053 47.2751 185.5255 0100268 45.6244 315.2705 12.17280489771009
| Epoch (UTC): | 06 October 2022 10:04:58 |
| Eccentricity: | 0.0100268 |
| inclination: | 47.2751° |
| perigee height: | 1524 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 185.5255° |
| argument of perigee: | 45.6244° |
| revolutions per day: | 12.17280489 |
| mean anomaly at epoch: | 315.2705° |
| orbit number at epoch: | 77100 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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