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 24357.74294387 .00081851 00000-0 19186-2 0 9998
2 33493 98.1749 64.0750 0007565 311.3214 48.7379 15.41750882867844
| Epoch (UTC): | 22 December 2024 17:49:50 |
| Eccentricity: | 0.0007565 |
| inclination: | 98.1749° |
| perigee height: | 436 km |
| apogee height: | 446 km |
| right ascension of ascending node: | 64.0750° |
| argument of perigee: | 311.3214° |
| revolutions per day: | 15.41750882 |
| mean anomaly at epoch: | 48.7379° |
| orbit number at epoch: | 86784 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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