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 23150.44128466 -.00000042 00000-0 43206-3 0 9994
2 00053 47.2736 177.6210 0097667 22.7147 337.7923 12.17300591799751
| Epoch (UTC): | 30 May 2023 10:35:26 |
| Eccentricity: | 0.0097667 |
| inclination: | 47.2736° |
| perigee height: | 1526 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 177.6210° |
| argument of perigee: | 22.7147° |
| revolutions per day: | 12.17300591 |
| mean anomaly at epoch: | 337.7923° |
| orbit number at epoch: | 79975 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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