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 68229U 26145.58335647 +.00000000 +00000-0 -24950-1 0 00001
2 68229 97.2855 23.6258 0001642 99.2381 208.2580 15.60297260 09
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001642 |
| inclination: | 97.2855° |
| perigee height: | 386 km |
| apogee height: | 388 km |
| right ascension of ascending node: | 23.6258° |
| argument of perigee: | 99.2381° |
| revolutions per day: | 15.60297260 |
| mean anomaly at epoch: | 208.2580° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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