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 68846U 26145.58335647 +.00000000 +00000-0 -84514-3 0 00000
2 68846 97.2847 160.3022 0000830 114.2768 162.9327 15.49222098 07
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0000830 |
| inclination: | 97.2847° |
| perigee height: | 418 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 160.3022° |
| argument of perigee: | 114.2768° |
| revolutions per day: | 15.49222098 |
| mean anomaly at epoch: | 162.9327° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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