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 26075.82006836 +.00000000 +00000-0 +19879-3 0 00001
2 33499 98.1185 356.8239 0006754 223.2903 136.7780 14.82857088 04
| Epoch (UTC): | 16 March 2026 19:40:53 |
| Eccentricity: | 0.0006754 |
| inclination: | 98.1185° |
| perigee height: | 616 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 356.8239° |
| argument of perigee: | 223.2903° |
| revolutions per day: | 14.82857088 |
| mean anomaly at epoch: | 136.7780° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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