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 43079U 26145.58462002 +.00000000 +00000-0 +12041-4 0 00003
2 43079 86.3961 331.6290 0002186 90.8436 269.3010 14.34217869 05
| Epoch (UTC): | 25 May 2026 14:01:51 |
| Eccentricity: | 0.0002186 |
| inclination: | 86.3961° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 331.6290° |
| argument of perigee: | 90.8436° |
| revolutions per day: | 14.34217869 |
| mean anomaly at epoch: | 269.3010° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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