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 68089U 26145.39770336 +.00000000 +00000-0 +39353-3 0 00006
2 68089 53.1578 182.1354 0001101 87.5253 272.5875 15.34403598 07
| Epoch (UTC): | 25 May 2026 09:32:41 |
| Eccentricity: | 0.0001101 |
| inclination: | 53.1578° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 182.1354° |
| argument of perigee: | 87.5253° |
| revolutions per day: | 15.34403598 |
| mean anomaly at epoch: | 272.5875° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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