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 53557U 26145.23622825 +.00000000 +00000-0 +20747-3 0 00009
2 53557 53.2137 80.4906 0001230 87.3450 272.7682 15.08824170 08
| Epoch (UTC): | 25 May 2026 05:40:10 |
| Eccentricity: | 0.0001230 |
| inclination: | 53.2137° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 80.4906° |
| argument of perigee: | 87.3450° |
| revolutions per day: | 15.08824170 |
| mean anomaly at epoch: | 272.7682° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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