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 33493U 09002B 23335.60676282 .00022091 00000-0 13188-2 0 9993
2 33493 98.2338 2.3138 0013950 197.7135 162.3609 15.11059519808982
| Epoch (UTC): | 01 December 2023 14:33:44 |
| Eccentricity: | 0.0013950 |
| inclination: | 98.2338° |
| perigee height: | 523 km |
| apogee height: | 542 km |
| right ascension of ascending node: | 2.3138° |
| argument of perigee: | 197.7135° |
| revolutions per day: | 15.11059519 |
| mean anomaly at epoch: | 162.3609° |
| orbit number at epoch: | 80898 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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