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 26038.30017809 +.00000000 +00000-0 +33092-3 0 00008
2 33499 98.1186 318.7368 0007990 2.5114 357.6138 14.82706537 03
| Epoch (UTC): | 07 February 2026 07:12:15 |
| Eccentricity: | 0.0007990 |
| inclination: | 98.1186° |
| perigee height: | 615 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 318.7368° |
| argument of perigee: | 2.5114° |
| revolutions per day: | 14.82706537 |
| mean anomaly at epoch: | 357.6138° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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