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 52668U 26145.37146980 +.00000000 +00000-0 +16633-4 0 00009
2 52668 53.2104 169.8834 0001393 51.1886 308.9230 15.08838651 08
| Epoch (UTC): | 25 May 2026 08:54:54 |
| Eccentricity: | 0.0001393 |
| inclination: | 53.2104° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 169.8834° |
| argument of perigee: | 51.1886° |
| revolutions per day: | 15.08838651 |
| mean anomaly at epoch: | 308.9230° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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