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 23038.46510393 -.00000060 00000-0 25360-3 0 9996
2 00053 47.2751 162.9625 0098708 53.9342 307.0542 12.17289740786110
| Epoch (UTC): | 07 February 2023 11:09:44 |
| Eccentricity: | 0.0098708 |
| inclination: | 47.2751° |
| perigee height: | 1525 km |
| apogee height: | 1683 km |
| right ascension of ascending node: | 162.9625° |
| argument of perigee: | 53.9342° |
| revolutions per day: | 12.17289740 |
| mean anomaly at epoch: | 307.0542° |
| orbit number at epoch: | 78611 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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