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 23342.29220320 -.00000016 00000-0 66477-3 0 9998
2 00053 47.2790 305.9155 0099489 232.0567 127.1198 12.17318267823124
| Epoch (UTC): | 08 December 2023 07:00:46 |
| Eccentricity: | 0.0099489 |
| inclination: | 47.2790° |
| perigee height: | 1525 km |
| apogee height: | 1683 km |
| right ascension of ascending node: | 305.9155° |
| argument of perigee: | 232.0567° |
| revolutions per day: | 12.17318267 |
| mean anomaly at epoch: | 127.1198° |
| orbit number at epoch: | 82312 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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