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 53169U 26145.45475927 +.00000000 +00000-0 -17899-4 0 00007
2 53169 53.2119 164.7654 0001019 66.5464 293.5635 15.08841809 09
| Epoch (UTC): | 25 May 2026 10:54:51 |
| Eccentricity: | 0.0001019 |
| inclination: | 53.2119° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 164.7654° |
| argument of perigee: | 66.5464° |
| revolutions per day: | 15.08841809 |
| mean anomaly at epoch: | 293.5635° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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