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 23335.39650421 -.00000070 00000-0 14123-3 0 9991
2 00053 47.2790 327.1833 0099748 211.6507 147.8257 12.17317663822288
| Epoch (UTC): | 01 December 2023 09:30:57 |
| Eccentricity: | 0.0099748 |
| inclination: | 47.2790° |
| perigee height: | 1524 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 327.1833° |
| argument of perigee: | 211.6507° |
| revolutions per day: | 12.17317663 |
| mean anomaly at epoch: | 147.8257° |
| orbit number at epoch: | 82228 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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