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 38245U 26145.59317514 +.00000000 +00000-0 +00000-0 0 00008
2 38245 0.0901 91.0414 0002615 348.5854 64.6979 1.00271003 09
| Epoch (UTC): | 25 May 2026 14:14:10 |
| Eccentricity: | 0.0002615 |
| inclination: | 0.0901° |
| perigee height: | 35776 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 91.0414° |
| argument of perigee: | 348.5854° |
| revolutions per day: | 1.00271003 |
| mean anomaly at epoch: | 64.6979° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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