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 33499U 09002H 23342.86276140 .00001319 00000-0 19112-3 0 9998
2 33499 98.1544 237.2778 0009561 33.9714 326.2106 14.77786805799856
| Epoch (UTC): | 08 December 2023 20:42:22 |
| Eccentricity: | 0.0009561 |
| inclination: | 98.1544° |
| perigee height: | 629 km |
| apogee height: | 643 km |
| right ascension of ascending node: | 237.2778° |
| argument of perigee: | 33.9714° |
| revolutions per day: | 14.77786805 |
| mean anomaly at epoch: | 326.2106° |
| orbit number at epoch: | 79985 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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