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 26069.98972360 +.00000000 +00000-0 +42794-3 0 00007
2 43678 98.1041 262.0798 0011929 122.9355 237.3016 14.99973503 08
| Epoch (UTC): | 10 March 2026 23:45:12 |
| Eccentricity: | 0.0011929 |
| inclination: | 98.1041° |
| perigee height: | 559 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 262.0798° |
| argument of perigee: | 122.9355° |
| revolutions per day: | 14.99973503 |
| mean anomaly at epoch: | 237.3016° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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