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 55310U 26145.41989367 +.00000000 +00000-0 +15075-4 0 00004
2 55310 69.9986 171.0738 0003701 267.8332 92.2403 14.98330450 09
| Epoch (UTC): | 25 May 2026 10:04:38 |
| Eccentricity: | 0.0003701 |
| inclination: | 69.9986° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 171.0738° |
| argument of perigee: | 267.8332° |
| revolutions per day: | 14.98330450 |
| mean anomaly at epoch: | 92.2403° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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