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 62570U 26145.48815944 +.00000000 +00000-0 +47458-3 0 00005
2 62570 42.9980 219.2262 0001006 273.3982 86.6755 15.27597768 03
| Epoch (UTC): | 25 May 2026 11:42:56 |
| Eccentricity: | 0.0001006 |
| inclination: | 42.9980° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 219.2262° |
| argument of perigee: | 273.3982° |
| revolutions per day: | 15.27597768 |
| mean anomaly at epoch: | 86.6755° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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