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 43678U 26073.92553884 +.00000000 +00000-0 +41671-3 0 00005
2 43678 98.1041 266.1775 0012350 110.9977 249.2568 14.99995111 07
| Epoch (UTC): | 14 March 2026 22:12:46 |
| Eccentricity: | 0.0012350 |
| inclination: | 98.1041° |
| perigee height: | 558 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 266.1775° |
| argument of perigee: | 110.9977° |
| revolutions per day: | 14.99995111 |
| mean anomaly at epoch: | 249.2568° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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