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 68701U 26145.58335647 +.00000000 +00000-0 -65603-1 0 00006
2 68701 53.1606 37.2523 0000714 129.5140 138.9054 15.37188660 06
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0000714 |
| inclination: | 53.1606° |
| perigee height: | 454 km |
| apogee height: | 455 km |
| right ascension of ascending node: | 37.2523° |
| argument of perigee: | 129.5140° |
| revolutions per day: | 15.37188660 |
| mean anomaly at epoch: | 138.9054° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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