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 26066.44046927 +.00000000 +00000-0 +32350-3 0 00003
2 33499 98.1186 347.3018 0006426 259.7148 100.3341 14.82819922 01
| Epoch (UTC): | 07 March 2026 10:34:16 |
| Eccentricity: | 0.0006426 |
| inclination: | 98.1186° |
| perigee height: | 616 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 347.3018° |
| argument of perigee: | 259.7148° |
| revolutions per day: | 14.82819922 |
| mean anomaly at epoch: | 100.3341° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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