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 68717U 26145.58335647 +.00000000 +00000-0 -49979-1 0 00001
2 68717 53.1604 37.0133 0000736 121.1263 264.4055 15.40064093 07
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0000736 |
| inclination: | 53.1604° |
| perigee height: | 445 km |
| apogee height: | 446 km |
| right ascension of ascending node: | 37.0133° |
| argument of perigee: | 121.1263° |
| revolutions per day: | 15.40064093 |
| mean anomaly at epoch: | 264.4055° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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