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 59727U 26145.39751910 +.00000000 +00000-0 +22684-4 0 00002
2 59727 53.1601 143.8075 0001231 85.7481 274.3661 15.31699792 07
| Epoch (UTC): | 25 May 2026 09:32:25 |
| Eccentricity: | 0.0001231 |
| inclination: | 53.1601° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 143.8075° |
| argument of perigee: | 85.7481° |
| revolutions per day: | 15.31699792 |
| mean anomaly at epoch: | 274.3661° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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