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 62886U 26145.52138708 +.00000000 +00000-0 +13225-2 0 00000
2 62886 42.9999 78.0333 0001220 53.9359 306.1622 15.70868180 01
| Epoch (UTC): | 25 May 2026 12:30:47 |
| Eccentricity: | 0.0001220 |
| inclination: | 42.9999° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 78.0333° |
| argument of perigee: | 53.9359° |
| revolutions per day: | 15.70868180 |
| mean anomaly at epoch: | 306.1622° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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