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 53555U 26145.50856016 +.00000000 +00000-0 +38708-3 0 00004
2 53555 53.2131 79.2671 0001535 90.3873 269.7295 15.08805947 03
| Epoch (UTC): | 25 May 2026 12:12:19 |
| Eccentricity: | 0.0001535 |
| inclination: | 53.2131° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 79.2671° |
| argument of perigee: | 90.3873° |
| revolutions per day: | 15.08805947 |
| mean anomaly at epoch: | 269.7295° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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