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 65017U 26145.42825602 +.00000000 +00000-0 +87609-3 0 00002
2 65017 53.1592 297.4168 0001387 113.0494 247.0653 15.30187502 03
| Epoch (UTC): | 25 May 2026 10:16:41 |
| Eccentricity: | 0.0001387 |
| inclination: | 53.1592° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 297.4168° |
| argument of perigee: | 113.0494° |
| revolutions per day: | 15.30187502 |
| mean anomaly at epoch: | 247.0653° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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