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 53639U 26145.66668980 +.00000000 +00000-0 +31612-2 0 00001
2 53639 53.2167 235.3497 0001241 65.2344 242.1085 15.31991191 09
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001241 |
| inclination: | 53.2167° |
| perigee height: | 469 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 235.3497° |
| argument of perigee: | 65.2344° |
| revolutions per day: | 15.31991191 |
| mean anomaly at epoch: | 242.1085° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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