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 68398U 26145.36293119 +.00000000 +00000-0 +70814-3 0 00002
2 68398 97.2854 287.8946 0001123 93.7222 266.4149 15.33465949 08
| Epoch (UTC): | 25 May 2026 08:42:37 |
| Eccentricity: | 0.0001123 |
| inclination: | 97.2854° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 287.8946° |
| argument of perigee: | 93.7222° |
| revolutions per day: | 15.33465949 |
| mean anomaly at epoch: | 266.4149° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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