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 22147.90324127 -.00000140 00000-0 -53513-3 0 9994
2 00053 47.2750 231.1206 0096933 17.4538 342.9547 12.17270485754982
| Epoch (UTC): | 27 May 2022 21:40:40 |
| Eccentricity: | 0.0096933 |
| inclination: | 47.2750° |
| perigee height: | 1527 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 231.1206° |
| argument of perigee: | 17.4538° |
| revolutions per day: | 12.17270485 |
| mean anomaly at epoch: | 342.9547° |
| orbit number at epoch: | 75498 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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