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 68479U 26145.62730916 +.00000000 +00000-0 +63809-3 0 00008
2 68479 97.7529 104.2402 0002018 48.3621 311.7771 14.92421819 01
| Epoch (UTC): | 25 May 2026 15:03:19 |
| Eccentricity: | 0.0002018 |
| inclination: | 97.7529° |
| perigee height: | 589 km |
| apogee height: | 592 km |
| right ascension of ascending node: | 104.2402° |
| argument of perigee: | 48.3621° |
| revolutions per day: | 14.92421819 |
| mean anomaly at epoch: | 311.7771° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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