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 55407U 26145.53324558 +.00000000 +00000-0 +49868-4 0 00006
2 55407 69.9993 230.7914 0003439 269.8108 90.2657 14.98333825 02
| Epoch (UTC): | 25 May 2026 12:47:52 |
| Eccentricity: | 0.0003439 |
| inclination: | 69.9993° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 230.7914° |
| argument of perigee: | 269.8108° |
| revolutions per day: | 14.98333825 |
| mean anomaly at epoch: | 90.2657° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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