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 26101.84646418 +.00000000 +00000-0 +32167-3 0 00003
2 33498 98.1492 46.4931 0009328 38.1783 322.0096 14.95286467 05
| Epoch (UTC): | 11 April 2026 20:18:54 |
| Eccentricity: | 0.0009328 |
| inclination: | 98.1492° |
| perigee height: | 575 km |
| apogee height: | 588 km |
| right ascension of ascending node: | 46.4931° |
| argument of perigee: | 38.1783° |
| revolutions per day: | 14.95286467 |
| mean anomaly at epoch: | 322.0096° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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