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 43873U 26145.31991323 +.00000000 +00000-0 +00000-0 0 00007
2 43873 55.6692 93.0882 0038028 198.4891 334.1413 2.00560673 09
| Epoch (UTC): | 25 May 2026 07:40:40 |
| Eccentricity: | 0.0038028 |
| inclination: | 55.6692° |
| perigee height: | 20081 km |
| apogee height: | 20283 km |
| right ascension of ascending node: | 93.0882° |
| argument of perigee: | 198.4891° |
| revolutions per day: | 2.00560673 |
| mean anomaly at epoch: | 334.1413° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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