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 23339.33690166 .00000004 00000-0 86880-3 0 9994
2 00053 47.2789 315.0302 0099547 223.3314 135.9614 12.17317991822768
| Epoch (UTC): | 05 December 2023 08:05:08 |
| Eccentricity: | 0.0099547 |
| inclination: | 47.2789° |
| perigee height: | 1525 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 315.0302° |
| argument of perigee: | 223.3314° |
| revolutions per day: | 12.17317991 |
| mean anomaly at epoch: | 135.9614° |
| orbit number at epoch: | 82276 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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