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 68908U 26145.58335647 +.00000000 +00000-0 +19980-3 0 00003
2 68908 97.2846 341.3742 0002185 84.7000 98.3268 15.33421497 03
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0002185 |
| inclination: | 97.2846° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 341.3742° |
| argument of perigee: | 84.7000° |
| revolutions per day: | 15.33421497 |
| mean anomaly at epoch: | 98.3268° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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