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 68642U 26144.80695633 +.00000000 +00000-0 +37306-4 0 00009
2 68642 88.9873 323.4210 0009788 72.9643 287.2585 13.59307647 01
| Epoch (UTC): | 24 May 2026 19:22:01 |
| Eccentricity: | 0.0009788 |
| inclination: | 88.9873° |
| perigee height: | 1031 km |
| apogee height: | 1045 km |
| right ascension of ascending node: | 323.4210° |
| argument of perigee: | 72.9643° |
| revolutions per day: | 13.59307647 |
| mean anomaly at epoch: | 287.2585° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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