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 68527U 26145.25225093 +.00000000 +00000-0 +72197-3 0 00006
2 68527 53.1587 130.2676 0001037 49.4866 310.6227 15.34403888 07
| Epoch (UTC): | 25 May 2026 06:03:14 |
| Eccentricity: | 0.0001037 |
| inclination: | 53.1587° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 130.2676° |
| argument of perigee: | 49.4866° |
| revolutions per day: | 15.34403888 |
| mean anomaly at epoch: | 310.6227° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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