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 68788U 26145.58335647 +.00000000 +00000-0 -16751-1 0 00001
2 68788 97.2852 182.4948 0001463 98.7318 176.0345 15.71762036 02
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001463 |
| inclination: | 97.2852° |
| perigee height: | 353 km |
| apogee height: | 355 km |
| right ascension of ascending node: | 182.4948° |
| argument of perigee: | 98.7318° |
| revolutions per day: | 15.71762036 |
| mean anomaly at epoch: | 176.0345° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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