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 43613U 26106.93217229 +.00000000 +00000-0 +70812-4 0 00002
2 43613 92.0009 274.4598 0003160 60.4682 299.6882 15.28265462 09
| Epoch (UTC): | 16 April 2026 22:22:19 |
| Eccentricity: | 0.0003160 |
| inclination: | 92.0009° |
| perigee height: | 479 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 274.4598° |
| argument of perigee: | 60.4682° |
| revolutions per day: | 15.28265462 |
| mean anomaly at epoch: | 299.6882° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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