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 23338.35180185 -.00000005 00000-0 77473-3 0 9990
2 00053 47.2788 318.0685 0099583 220.4151 138.9207 12.17317874822649
| Epoch (UTC): | 04 December 2023 08:26:35 |
| Eccentricity: | 0.0099583 |
| inclination: | 47.2788° |
| perigee height: | 1525 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 318.0685° |
| argument of perigee: | 220.4151° |
| revolutions per day: | 12.17317874 |
| mean anomaly at epoch: | 138.9207° |
| orbit number at epoch: | 82264 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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