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 33492U 26150.27463373 +.00000000 +00000-0 +17109-3 0 00004
2 33492 98.0875 261.5820 0001670 95.6093 264.5302 14.67537679 07
| Epoch (UTC): | 30 May 2026 06:35:28 |
| Eccentricity: | 0.0001670 |
| inclination: | 98.0875° |
| perigee height: | 668 km |
| apogee height: | 670 km |
| right ascension of ascending node: | 261.5820° |
| argument of perigee: | 95.6093° |
| revolutions per day: | 14.67537679 |
| mean anomaly at epoch: | 264.5302° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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