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 55649U 26145.53045623 +.00000000 +00000-0 +12103-4 0 00009
2 55649 69.9994 350.6234 0002651 269.1842 90.9014 14.98330590 01
| Epoch (UTC): | 25 May 2026 12:43:51 |
| Eccentricity: | 0.0002651 |
| inclination: | 69.9994° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 350.6234° |
| argument of perigee: | 269.1842° |
| revolutions per day: | 14.98330590 |
| mean anomaly at epoch: | 90.9014° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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