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 53888U 26145.66668980 +.00000000 +00000-0 +19380-2 0 00005
2 53888 53.2158 316.2089 0000838 37.6817 217.6242 15.82944588 06
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0000838 |
| inclination: | 53.2158° |
| perigee height: | 322 km |
| apogee height: | 323 km |
| right ascension of ascending node: | 316.2089° |
| argument of perigee: | 37.6817° |
| revolutions per day: | 15.82944588 |
| mean anomaly at epoch: | 217.6242° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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