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 59723U 26145.38573722 +.00000000 +00000-0 +93016-5 0 00008
2 59723 53.1604 143.7378 0001214 86.3616 273.7524 15.30190034 04
| Epoch (UTC): | 25 May 2026 09:15:27 |
| Eccentricity: | 0.0001214 |
| inclination: | 53.1604° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 143.7378° |
| argument of perigee: | 86.3616° |
| revolutions per day: | 15.30190034 |
| mean anomaly at epoch: | 273.7524° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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