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 43189U 26145.38339913 +.00000000 +00000-0 +22691-3 0 00008
2 43189 97.5414 50.5797 0012043 86.9657 273.2954 15.16379794 05
| Epoch (UTC): | 25 May 2026 09:12:05 |
| Eccentricity: | 0.0012043 |
| inclination: | 97.5414° |
| perigee height: | 508 km |
| apogee height: | 525 km |
| right ascension of ascending node: | 50.5797° |
| argument of perigee: | 86.9657° |
| revolutions per day: | 15.16379794 |
| mean anomaly at epoch: | 273.2954° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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