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 62506U 26145.60101926 +.00000000 +00000-0 +54233-3 0 00005
2 62506 43.0030 196.0672 0002055 267.0569 93.0048 15.27587528 03
| Epoch (UTC): | 25 May 2026 14:25:28 |
| Eccentricity: | 0.0002055 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 196.0672° |
| argument of perigee: | 267.0569° |
| revolutions per day: | 15.27587528 |
| mean anomaly at epoch: | 93.0048° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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