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 68505U 26145.61504904 +.00000000 +00000-0 +42626-3 0 00007
2 68505 97.7587 104.1399 0007007 111.7338 248.4626 14.90926785 07
| Epoch (UTC): | 25 May 2026 14:45:40 |
| Eccentricity: | 0.0007007 |
| inclination: | 97.7587° |
| perigee height: | 590 km |
| apogee height: | 600 km |
| right ascension of ascending node: | 104.1399° |
| argument of perigee: | 111.7338° |
| revolutions per day: | 14.90926785 |
| mean anomaly at epoch: | 248.4626° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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