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 68704U 26145.58335647 +.00000000 +00000-0 -51843-1 0 00000
2 68704 53.1594 37.2626 0001334 111.8948 150.3814 15.38797618 00
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001334 |
| inclination: | 53.1594° |
| perigee height: | 449 km |
| apogee height: | 451 km |
| right ascension of ascending node: | 37.2626° |
| argument of perigee: | 111.8948° |
| revolutions per day: | 15.38797618 |
| mean anomaly at epoch: | 150.3814° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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