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 15333U 26099.54732262 +.00000000 +00000-0 -64959-4 0 00003
2 15333 71.0278 191.6978 0020425 339.6255 20.4050 14.14511690 02
| Epoch (UTC): | 09 April 2026 13:08:08 |
| Eccentricity: | 0.0020425 |
| inclination: | 71.0278° |
| perigee height: | 829 km |
| apogee height: | 859 km |
| right ascension of ascending node: | 191.6978° |
| argument of perigee: | 339.6255° |
| revolutions per day: | 14.14511690 |
| mean anomaly at epoch: | 20.4050° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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