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 52698U 26145.43264906 +.00000000 +00000-0 +72644-4 0 00002
2 52698 53.2119 164.5999 0001193 83.0373 277.0755 15.08844343 07
| Epoch (UTC): | 25 May 2026 10:23:00 |
| Eccentricity: | 0.0001193 |
| inclination: | 53.2119° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 164.5999° |
| argument of perigee: | 83.0373° |
| revolutions per day: | 15.08844343 |
| mean anomaly at epoch: | 277.0755° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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