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 26037.79137355 +.00000000 +00000-0 +66360-3 0 00002
2 33498 98.1436 339.9917 0006789 234.0945 125.9645 14.94607416 02
| Epoch (UTC): | 06 February 2026 18:59:34 |
| Eccentricity: | 0.0006789 |
| inclination: | 98.1436° |
| perigee height: | 579 km |
| apogee height: | 588 km |
| right ascension of ascending node: | 339.9917° |
| argument of perigee: | 234.0945° |
| revolutions per day: | 14.94607416 |
| mean anomaly at epoch: | 125.9645° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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