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 53735U 26145.64468278 +.00000000 +00000-0 +52844-4 0 00006
2 53735 53.2163 278.4681 0001348 94.0591 266.0555 15.08841629 08
| Epoch (UTC): | 25 May 2026 15:28:20 |
| Eccentricity: | 0.0001348 |
| inclination: | 53.2163° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 278.4681° |
| argument of perigee: | 94.0591° |
| revolutions per day: | 15.08841629 |
| mean anomaly at epoch: | 266.0555° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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