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 59218U 26145.35285139 +.00000000 +00000-0 +24504-4 0 00001
2 59218 53.1604 158.0946 0001203 92.9348 267.1792 15.34384257 06
| Epoch (UTC): | 25 May 2026 08:28:06 |
| Eccentricity: | 0.0001203 |
| inclination: | 53.1604° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 158.0946° |
| argument of perigee: | 92.9348° |
| revolutions per day: | 15.34384257 |
| mean anomaly at epoch: | 267.1792° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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