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 53975U 26145.49608087 +.00000000 +00000-0 +28588-4 0 00007
2 53975 53.2118 233.8987 0001117 82.4160 277.6959 15.08834738 04
| Epoch (UTC): | 25 May 2026 11:54:21 |
| Eccentricity: | 0.0001117 |
| inclination: | 53.2118° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 233.8987° |
| argument of perigee: | 82.4160° |
| revolutions per day: | 15.08834738 |
| mean anomaly at epoch: | 277.6959° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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