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 68338U 26145.58335647 +.00000000 +00000-0 +74255-3 0 00006
2 68338 53.1597 346.6726 0001323 81.7039 162.5206 15.35363509 03
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001323 |
| inclination: | 53.1597° |
| perigee height: | 459 km |
| apogee height: | 461 km |
| right ascension of ascending node: | 346.6726° |
| argument of perigee: | 81.7039° |
| revolutions per day: | 15.35363509 |
| mean anomaly at epoch: | 162.5206° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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