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 62555U 26145.42213102 +.00000000 +00000-0 +13926-2 0 00002
2 62555 43.0006 37.0902 0001566 258.2717 101.7975 15.70905709 02
| Epoch (UTC): | 25 May 2026 10:07:52 |
| Eccentricity: | 0.0001566 |
| inclination: | 43.0006° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 37.0902° |
| argument of perigee: | 258.2717° |
| revolutions per day: | 15.70905709 |
| mean anomaly at epoch: | 101.7975° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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