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 53530U 26145.09549794 +.00000000 +00000-0 -39458-4 0 00008
2 53530 53.2141 91.3395 0001628 110.0702 250.0466 15.08841881 09
| Epoch (UTC): | 25 May 2026 02:17:31 |
| Eccentricity: | 0.0001628 |
| inclination: | 53.2141° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 91.3395° |
| argument of perigee: | 110.0702° |
| revolutions per day: | 15.08841881 |
| mean anomaly at epoch: | 250.0466° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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