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 65938U 26145.65191427 +.00000000 +00000-0 +39382-3 0 00005
2 65938 97.6440 225.9462 0013028 218.8373 141.1924 15.15968171 05
| Epoch (UTC): | 25 May 2026 15:38:45 |
| Eccentricity: | 0.0013028 |
| inclination: | 97.6440° |
| perigee height: | 509 km |
| apogee height: | 527 km |
| right ascension of ascending node: | 225.9462° |
| argument of perigee: | 218.8373° |
| revolutions per day: | 15.15968171 |
| mean anomaly at epoch: | 141.1924° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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