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 68436U 26145.40946715 +.00000000 +00000-0 +20165-3 0 00001
2 68436 97.4530 104.1916 0004312 109.6299 250.5401 15.18001356 02
| Epoch (UTC): | 25 May 2026 09:49:37 |
| Eccentricity: | 0.0004312 |
| inclination: | 97.4530° |
| perigee height: | 509 km |
| apogee height: | 515 km |
| right ascension of ascending node: | 104.1916° |
| argument of perigee: | 109.6299° |
| revolutions per day: | 15.18001356 |
| mean anomaly at epoch: | 250.5401° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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