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 68342U 26145.55784191 +.00000000 +00000-0 +14938-2 0 00001
2 68342 53.1587 347.7405 0000787 94.7713 265.3386 15.49364780 07
| Epoch (UTC): | 25 May 2026 13:23:17 |
| Eccentricity: | 0.0000787 |
| inclination: | 53.1587° |
| perigee height: | 418 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 347.7405° |
| argument of perigee: | 94.7713° |
| revolutions per day: | 15.49364780 |
| mean anomaly at epoch: | 265.3386° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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