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 68659U 26144.56440690 +.00000000 +00000-0 -57326-4 0 00006
2 68659 86.4994 51.8746 0003030 67.4255 292.7206 13.35106587 09
| Epoch (UTC): | 24 May 2026 13:32:44 |
| Eccentricity: | 0.0003030 |
| inclination: | 86.4994° |
| perigee height: | 1125 km |
| apogee height: | 1130 km |
| right ascension of ascending node: | 51.8746° |
| argument of perigee: | 67.4255° |
| revolutions per day: | 13.35106587 |
| mean anomaly at epoch: | 292.7206° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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