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 26073.59199832 +.00000000 +00000-0 +17945-3 0 00004
2 43678 98.1039 265.8299 0012295 112.3342 247.9185 14.99988445 03
| Epoch (UTC): | 14 March 2026 14:12:28 |
| Eccentricity: | 0.0012295 |
| inclination: | 98.1039° |
| perigee height: | 558 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 265.8299° |
| argument of perigee: | 112.3342° |
| revolutions per day: | 14.99988445 |
| mean anomaly at epoch: | 247.9185° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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