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 24257.51005848 .00017894 00000-0 20014-2 0 9997
2 33498 98.1126 173.5342 0011746 114.7231 245.5208 14.86924597843218
| Epoch (UTC): | 13 September 2024 12:14:29 |
| Eccentricity: | 0.0011746 |
| inclination: | 98.1126° |
| perigee height: | 599 km |
| apogee height: | 616 km |
| right ascension of ascending node: | 173.5342° |
| argument of perigee: | 114.7231° |
| revolutions per day: | 14.86924597 |
| mean anomaly at epoch: | 245.5208° |
| orbit number at epoch: | 84321 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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