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 33498U 09002G 23335.31428210 .00006493 00000-0 79700-3 0 9993
2 33498 98.1250 240.8846 0009735 342.2935 17.7937 14.83401861800590
| Epoch (UTC): | 01 December 2023 07:32:33 |
| Eccentricity: | 0.0009735 |
| inclination: | 98.1250° |
| perigee height: | 612 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 240.8846° |
| argument of perigee: | 342.2935° |
| revolutions per day: | 14.83401861 |
| mean anomaly at epoch: | 17.7937° |
| orbit number at epoch: | 80059 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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