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 68658U 26144.56937330 +.00000000 +00000-0 -46598-3 0 00005
2 68658 86.4938 51.8443 0001796 64.0295 296.1030 13.34697661 04
| Epoch (UTC): | 24 May 2026 13:39:53 |
| Eccentricity: | 0.0001796 |
| inclination: | 86.4938° |
| perigee height: | 1128 km |
| apogee height: | 1130 km |
| right ascension of ascending node: | 51.8443° |
| argument of perigee: | 64.0295° |
| revolutions per day: | 13.34697661 |
| mean anomaly at epoch: | 296.1030° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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