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 68778U 26145.58335647 +.00000000 +00000-0 -25392-1 0 00001
2 68778 97.2848 182.4385 0001700 76.7725 59.7880 15.60379856 06
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001700 |
| inclination: | 97.2848° |
| perigee height: | 385 km |
| apogee height: | 388 km |
| right ascension of ascending node: | 182.4385° |
| argument of perigee: | 76.7725° |
| revolutions per day: | 15.60379856 |
| mean anomaly at epoch: | 59.7880° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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