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 55960U 26145.21027237 +.00000000 +00000-0 +48511-4 0 00003
2 55960 70.0001 71.5677 0003045 269.1347 90.9463 14.98332311 08
| Epoch (UTC): | 25 May 2026 05:02:47 |
| Eccentricity: | 0.0003045 |
| inclination: | 70.0001° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 71.5677° |
| argument of perigee: | 269.1347° |
| revolutions per day: | 14.98332311 |
| mean anomaly at epoch: | 90.9463° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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