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 07493U 74083B 23335.62488366 .00000167 00000-0 89651-4 0 9991
2 07493 81.1618 13.2962 0079156 289.0904 70.1705 14.07741577520261
| Epoch (UTC): | 01 December 2023 14:59:49 |
| Eccentricity: | 0.0079156 |
| inclination: | 81.1618° |
| perigee height: | 810 km |
| apogee height: | 924 km |
| right ascension of ascending node: | 13.2962° |
| argument of perigee: | 289.0904° |
| revolutions per day: | 14.07741577 |
| mean anomaly at epoch: | 70.1705° |
| orbit number at epoch: | 52026 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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