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 52697U 26145.35632777 +.00000000 +00000-0 +40605-4 0 00009
2 52697 53.2127 164.9519 0001123 83.3623 276.7497 15.08834626 03
| Epoch (UTC): | 25 May 2026 08:33:06 |
| Eccentricity: | 0.0001123 |
| inclination: | 53.2127° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 164.9519° |
| argument of perigee: | 83.3623° |
| revolutions per day: | 15.08834626 |
| mean anomaly at epoch: | 276.7497° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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