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 68705U 26145.58335647 +.00000000 +00000-0 +20446-2 0 00006
2 68705 53.1593 37.3241 0000934 124.6262 106.7386 15.35350968 09
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0000934 |
| inclination: | 53.1593° |
| perigee height: | 459 km |
| apogee height: | 461 km |
| right ascension of ascending node: | 37.3241° |
| argument of perigee: | 124.6262° |
| revolutions per day: | 15.35350968 |
| mean anomaly at epoch: | 106.7386° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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