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 68559U 26145.50003470 +.00000000 +00000-0 +19876-2 0 00006
2 68559 53.1587 5.1798 0000867 102.4443 255.8227 15.34353375 03
| Epoch (UTC): | 25 May 2026 12:00:02 |
| Eccentricity: | 0.0000867 |
| inclination: | 53.1587° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 5.1798° |
| argument of perigee: | 102.4443° |
| revolutions per day: | 15.34353375 |
| mean anomaly at epoch: | 255.8227° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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