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 20433U 26076.25144043 +.00000000 +00000-0 +96551-4 0 00009
2 20433 74.0340 246.7916 0040706 315.5772 218.0414 14.37506922 03
| Epoch (UTC): | 17 March 2026 06:02:04 |
| Eccentricity: | 0.0040706 |
| inclination: | 74.0340° |
| perigee height: | 738 km |
| apogee height: | 796 km |
| right ascension of ascending node: | 246.7916° |
| argument of perigee: | 315.5772° |
| revolutions per day: | 14.37506922 |
| mean anomaly at epoch: | 218.0414° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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