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 39022U 26145.59464847 +.00000000 +00000-0 +00000-0 0 00004
2 39022 1.2094 84.4254 0003929 336.2611 91.4610 1.00271759 09
| Epoch (UTC): | 25 May 2026 14:16:17 |
| Eccentricity: | 0.0003929 |
| inclination: | 1.2094° |
| perigee height: | 35770 km |
| apogee height: | 35803 km |
| right ascension of ascending node: | 84.4254° |
| argument of perigee: | 336.2611° |
| revolutions per day: | 1.00271759 |
| mean anomaly at epoch: | 91.4610° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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