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 55930U 26145.54413178 +.00000000 +00000-0 +45692-3 0 00005
2 55930 70.0010 90.6285 0003472 270.2063 89.8698 14.98338102 05
| Epoch (UTC): | 25 May 2026 13:03:32 |
| Eccentricity: | 0.0003472 |
| inclination: | 70.0010° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 90.6285° |
| argument of perigee: | 270.2063° |
| revolutions per day: | 14.98338102 |
| mean anomaly at epoch: | 89.8698° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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