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 26073.86319244 +.00000000 +00000-0 +26768-3 0 00008
2 33499 98.1183 354.8369 0006665 230.3696 129.6929 14.82852034 05
| Epoch (UTC): | 14 March 2026 20:42:59 |
| Eccentricity: | 0.0006665 |
| inclination: | 98.1183° |
| perigee height: | 616 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 354.8369° |
| argument of perigee: | 230.3696° |
| revolutions per day: | 14.82852034 |
| mean anomaly at epoch: | 129.6929° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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