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 24260.67728002 .00053927 00000-0 20374-2 0 9993
2 33493 98.1941 316.5794 0009584 286.5906 73.4278 15.26761283852976
| Epoch (UTC): | 16 September 2024 16:15:16 |
| Eccentricity: | 0.0009584 |
| inclination: | 98.1941° |
| perigee height: | 479 km |
| apogee height: | 492 km |
| right ascension of ascending node: | 316.5794° |
| argument of perigee: | 286.5906° |
| revolutions per day: | 15.26761283 |
| mean anomaly at epoch: | 73.4278° |
| orbit number at epoch: | 85297 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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