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 53903U 26145.50397142 +.00000000 +00000-0 +65492-3 0 00001
2 53903 53.2119 339.0923 0001370 94.2472 265.8677 15.08812360 06
| Epoch (UTC): | 25 May 2026 12:05:43 |
| Eccentricity: | 0.0001370 |
| inclination: | 53.2119° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 339.0923° |
| argument of perigee: | 94.2472° |
| revolutions per day: | 15.08812360 |
| mean anomaly at epoch: | 265.8677° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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