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 38254U 26140.58976865 +.00000000 +00000-0 +00000-0 0 00002
2 38254 6.5887 57.6900 0002522 352.8327 23.5799 1.00271709 08
| Epoch (UTC): | 20 May 2026 14:09:16 |
| Eccentricity: | 0.0002522 |
| inclination: | 6.5887° |
| perigee height: | 35776 km |
| apogee height: | 35797 km |
| right ascension of ascending node: | 57.6900° |
| argument of perigee: | 352.8327° |
| revolutions per day: | 1.00271709 |
| mean anomaly at epoch: | 23.5799° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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