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 33499U 26159.48593558 +.00000000 +00000-0 +18948-3 0 00004
2 33499 98.1193 81.7904 0007063 328.5178 31.5611 14.83102467 03
| Epoch (UTC): | 08 June 2026 11:39:44 |
| Eccentricity: | 0.0007063 |
| inclination: | 98.1193° |
| perigee height: | 615 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 81.7904° |
| argument of perigee: | 328.5178° |
| revolutions per day: | 14.83102467 |
| mean anomaly at epoch: | 31.5611° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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