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 68486U 26145.37339056 +.00000000 +00000-0 +17439-3 0 00006
2 68486 97.7569 103.9767 0002460 69.1652 290.9830 14.91884278 04
| Epoch (UTC): | 25 May 2026 08:57:40 |
| Eccentricity: | 0.0002460 |
| inclination: | 97.7569° |
| perigee height: | 590 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 103.9767° |
| argument of perigee: | 69.1652° |
| revolutions per day: | 14.91884278 |
| mean anomaly at epoch: | 290.9830° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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