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 55928U 26145.34824998 +.00000000 +00000-0 -16768-3 0 00009
2 55928 69.9990 111.0226 0003125 271.9318 88.1483 14.98338672 01
| Epoch (UTC): | 25 May 2026 08:21:28 |
| Eccentricity: | 0.0003125 |
| inclination: | 69.9990° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 111.0226° |
| argument of perigee: | 271.9318° |
| revolutions per day: | 14.98338672 |
| mean anomaly at epoch: | 88.1483° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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