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 68059U 26145.46345763 +.00000000 +00000-0 +83078-3 0 00006
2 68059 53.1604 51.7817 0001278 90.7226 269.3923 15.34409862 08
| Epoch (UTC): | 25 May 2026 11:07:22 |
| Eccentricity: | 0.0001278 |
| inclination: | 53.1604° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 51.7817° |
| argument of perigee: | 90.7226° |
| revolutions per day: | 15.34409862 |
| mean anomaly at epoch: | 269.3923° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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