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 62026U 26145.35793301 +.00000000 +00000-0 +44249-3 0 00004
2 62026 53.1573 171.9671 0000946 84.3471 275.7638 15.30213261 02
| Epoch (UTC): | 25 May 2026 08:35:25 |
| Eccentricity: | 0.0000946 |
| inclination: | 53.1573° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 171.9671° |
| argument of perigee: | 84.3471° |
| revolutions per day: | 15.30213261 |
| mean anomaly at epoch: | 275.7638° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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