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 25165.55011123 .00004442 00000-0 44513-3 0 9999
2 33498 98.1249 94.8585 0007707 309.6419 50.4118 14.91882900884016
| Epoch (UTC): | 14 June 2025 13:12:09 |
| Eccentricity: | 0.0007707 |
| inclination: | 98.1249° |
| perigee height: | 586 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 94.8585° |
| argument of perigee: | 309.6419° |
| revolutions per day: | 14.91882900 |
| mean anomaly at epoch: | 50.4118° |
| orbit number at epoch: | 88401 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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