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 is defined by the following mean orbital elements,
1 33498U 26072.33261388 +.00000000 +00000-0 +49224-3 0 00005
2 33498 98.1466 15.8352 0010017 119.5813 240.6406 14.94983530 02
| Epoch (UTC): | 13 March 2026 07:58:57 |
| Eccentricity: | 0.0010017 |
| inclination: | 98.1466° |
| perigee height: | 575 km |
| apogee height: | 589 km |
| right ascension of ascending node: | 15.8352° |
| argument of perigee: | 119.5813° |
| revolutions per day: | 14.94983530 |
| mean anomaly at epoch: | 240.6406° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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