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 55937U 26145.22702747 +.00000000 +00000-0 +25271-4 0 00002
2 55937 69.9998 91.5259 0003310 266.6516 93.4265 14.98333301 05
| Epoch (UTC): | 25 May 2026 05:26:55 |
| Eccentricity: | 0.0003310 |
| inclination: | 69.9998° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 91.5259° |
| argument of perigee: | 266.6516° |
| revolutions per day: | 14.98333301 |
| mean anomaly at epoch: | 93.4265° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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