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 52681U 26145.44966338 +.00000000 +00000-0 +92709-5 0 00008
2 52681 53.2133 159.5301 0001012 68.7040 291.4060 15.08841795 04
| Epoch (UTC): | 25 May 2026 10:47:30 |
| Eccentricity: | 0.0001012 |
| inclination: | 53.2133° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 159.5301° |
| argument of perigee: | 68.7040° |
| revolutions per day: | 15.08841795 |
| mean anomaly at epoch: | 291.4060° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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