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 62326U 26145.62085759 +.00000000 +00000-0 +39868-4 0 00000
2 62326 86.4992 350.7993 0001364 86.9020 273.2270 13.24407959 01
| Epoch (UTC): | 25 May 2026 14:54:02 |
| Eccentricity: | 0.0001364 |
| inclination: | 86.4992° |
| perigee height: | 1167 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 350.7993° |
| argument of perigee: | 86.9020° |
| revolutions per day: | 13.24407959 |
| mean anomaly at epoch: | 273.2270° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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